Vortex turbine engine

ABSTRACT

The apparatus relates generally by using a low pressure kinetic ambient air medium that being drawn in, and then being able to by generating this medium to a very high kinetic moving air pressure. Turning this air speed to form a vortex and then split the air-radiation heat from the cold air stream. The said vortex would then have a temperatures separate effect within its vortex. The said separate effect would separate its air-radiation heat from its air stream. The said separated air-radiation heat would via an adjustable hot outlet valve and would increase its hot heat value output. This apparatus is a non-vapor compression that is the said apparatus uses no refrigerant of any kind. The said air-radiation heat with its increasing heat value output would have a cold water conversion to steam. The said steam is then use to drive a steam turbine producing toque for the user. The said apparatus split-system with its temperatures separation effect would be useful for its non-vapor compression, heating and cooling and refrigeration systems. The said steam would have a steam to warm water conversion and then a warm water-to-steam conversion, therefore commencing cycle thereat.

REFERENCE TO MICROFICHE APPENDIX

Not applicable.

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT

Not applicable.

CROSS-REFERENCE TO RELATED APPLICATIONS References Cited: U.S PatentDocuments

-   U.S. Pat. No. 746,388—Inventor: Schefler * Dec. 8, 1903-   U.S. Pat. No. 777,313—Inventor: Smith * Dec. 13, 1904-   U.S. Pat. No. 1,952,281—Inventor: Ranque * Mar. 27, 1934-   U.S. Pat. No. 1,961,179—Inventor Drier * Jun. 5, 1934-   U.S. Pat. No. 2,488,467—Inventor: S. De Lisio * Nov. 15, 1949-   U.S. Pat. No. 2,672,806—Inventor: Vehige * Mar. 23, 1954-   U.S. Pat. No. 3,358,748—Inventor: Christopher * Dec. 8, 1967-   U.S. Pat. No. 3,366,363—Inventor: Hogan * Jan. 30, 1968-   U.S. Pat. No. 4,240,261—Inventor: Inglis * Dec. 23, 1980-   U.S. Pat. No. 4,494,009—Inventor: Yukl * Jan. 15, 1985-   U.S. Pat. No. 4,593,429—Inventor: Dyson * Jun. 10, 1986-   U.S. Pat. No. 4,594,084—Inventor: Lopez * Jun. 10, 1986-   U.S. Pat. No. 4,856,968—Inventor: Armbruster * Aug. 15, 1989-   U.S. Pat. No. 4,907,552—Inventor: Martin * Mar. 13, 1990-   U.S. Pat. No. 4,962,642—Inventor: Kim * Oct. 16, 1990-   U.S. Pat. No. 7,086,823—Inventor: Michaud * Aug. 8, 2006-   Application 2013/1401284—Inventor: Van Valkenburgh et al * Aug. 28,    2013

OTHER PUBLICATIONS

-   Michaud, L. M., 1999: Vortex process for capturing mechanical energy    during upward heat-convection in the atmosphere. Applied Energy,    62/4, 241*251.-   Michaud, L. M., 2000: Thermodynamic cycle of the atmospheric upward    heat convection process. Meteorol. Atmos. Phys. 72, 29*46.-   The Ranque-Hilsch Vortex Tube—Giorgio De Vera—May 10, 2010-   Engenharia Termica (Thermal Engineering), Vol. 11 * No. 1-2 * June    and December 2012-p. 85-92-   Energy Savings Potential and RD&D Opportunities for    Non-Vapor-Compression HVAC Technologies, U.S. Department of Energy    Office of Energy Efficiency and Renewable Energy Building    Technologies Office—March 2014

INDUSTRIAL APPLICABILITY

The Vortex Turbine Engine also known as apparatus-(A) 02 is a usefulpowertrain for eliminating range anxiety in mobile or power movingunits. The said (A) 02 is a useful powertrain in all kinds of vehicles;cars, vans, auto trucks, buses, or watercrafts. Be a useful powertrainfor the residential, commercial or industrial uses.

The apparatus-(A) 02 uses no water for its non-vapor compressionheating, cooling and refrigeration embodiment portion, and would beknown as the apparatus-NVCHACR-(NV) 02NV (non-vapor compression,heating, cooling and refrigeration) systems. The said (NV) 02NVsplit-system with its temperatures separation effect would be useful forits non-vapor compression, heating and cooling and refrigerationsystems. Although the present invention references the said (A) 02,other are within the scope and can equally benefits from the invention.The water the said does use is use to have and cold water to steamconversion, that being used for the steam turbine-(M) 24.

The apparatus-(A) 02 is useful for its non-polluting energy-efficientsystem. The said (A) 02 uses no fuel, like oil or gas, the only energythat being used is the electricity for the cylinder motor. Of the mainportion of the embodiment there will be only two moving embodiments.With a minimum of moving embodiments this translates into virtuallylittle maintenance.

The apparatus-(A) 02 application generally relates to a two or aplurality of the narrowing spiral tube-(B) 04 and by using the narrowingvortex cylinder-(G) 14 for its temperatures separation effect, havingits air-radiation heat separate from its air stream. The separated hightemperatures would be used to have a water-to-steam conversion. The saidsteam would be used in the steam turbine-(M) 24, producing torque forits applications needs. The said (A) 02 temperatures separation effectwould be useful for its non-vapor compression, heating and cooling andrefrigeration systems.

TECHNICAL FIELD

The apparatus-(A) 02 relates generally by using a low pressure kineticambient air medium that being drawn in, then being able to by generatingthis medium to a very high kinetic moving air pressure. The said (A) 02is a closed area that would have an opening at each one of the narrowingspiral tube-(B) 04 at its ambient air intakes, with an opening at theradiation boiler chamber-(H) 16 at its air heat outlet, and with anopening at the flash steam cooling air chamber-(K) 20 at its cold airoutlet.

The air stream gains velocity while the circumventing air move forward,the air is drawn circumventing through its one of the one, two or aplurality of the said narrowing spiral tube-(B) 04 with its ingrainedvortex nozzle and then through its one of the two or a plurality of thenarrowing volute generator-(C) 06 with its ingrained vortex nozzle.There would be the same amount of numbers of the said (B) 04 with itsvortex nozzle as there are in numbers of the said (C) 06 with its vortexnozzle.

Each one of the said narrowing spiral tube-(B) 04 vortex nozzle would beconnected to its one of the said narrowing volute generator-(C) 06. Eachone of the said (B) 04 and along with each one of the said (C) 06, allof these would have a converging portion that would have a greaterdiameter than the diverging portion, to enhance its vortices intensity.The drawing of the air causes a low pressure in front of the highpressured regions, causing the molecules to accelerate toward the lowpressure regions.

The said narrowing spiral tube-(B) 04 with its vortex nozzle, the saidnarrowing volute generator-(C) 06 with its vortex nozzle, the fanchamber-(D) 08, and their air stream is being drawn into the saidapparatus-(A) 02 by the cyclone narrowing cylinder-(E) 10. The said (E)10 joined to and would lay in-between the said (D) 08 within its innerwall. The said (E) 10 spin on its horizontal-axis between the diameterinterior side walls of the said (D) 08. Then the said (E) 10 drives theair stream to via the advance narrowing chamber-(F) 12.

The said advance narrowing chamber-(F) 12 having an narrowing tube airoutlets with its high speed air stream to via and to advance, generate,and helps to form a vortex within the narrowing vortex cylinder-(G) 14giving the said (G) 14 with continuous air stream. The said (G) 14 therewould be a temperature separation effect, separating the air-radiationheat from its air stream. The said (G) 14 cold air stream would via thecold air cooling chamber-(J) 18. The said (G) 14 with its saidair-radiation heat to via its hot narrowing tube outlet and then itsair-radiation heat to via its adjustable hot outlet valve and then thesaid air-radiation heat would via the said radiation boiler chamber-(H)16.

Using the said narrowing vortex cylinder-(G) 14 with its air-radiationheat on the cold/warm water in effect, would cause a warm water-to-steamconversion within the radiation steam line-(L) 22. The said (L) 22 withits steam, the steam would via the steam turbine-(M) 24. The said steamwould drive the said (M) 24. The said (M) 24 uses the steam to force thedrive shaft-(N) 26 to rotate on its horizontal-axis producing torque.

The said narrowing vortex cylinder-(G) 14 with its inner cold end, itscold air being used with the return water line-(P) 28, the cold airstream would absorb the latent heat energy from the hot water comingfrom the said steam turbine-(M) 24, having the hot water-to-warm waterconversion. The cold temperature in effect would return the hot watercoming from the said (M) 24 that would via the said (P) 28, to have aconversion from hot water to warm water therefore commence the warmwater back to-steam within the said radiation steam line-(L) 22 having aconversion cycles thereat. The said (P) 28 uses the warm water pump-(R)30 to pump the warm water to via the said (L) 22 for the said cyclethereat.

The air-radiation heat emerging from today's vortex tube. The saidtoday's vortex tube outer hot end can reach temperatures as high as+200° C. and the air emerging from its inner cold end can reach −50° C.The said narrowing vortex cylinder-(G) 14 would separate its air streaminto an air-radiation heat stream and a cold stream. Each one of thesaid narrowing spiral tube-(B) 04 narrowing passageways, along with eachone of the said narrowing volute generator-(C) 06 narrowing passageways,the said advance narrowing chamber-(F) 12 narrowing tube air outlets,the said (G) 14, each one of these would have a converging portion thatwould have a greater diameter than the diverging portion, as these wouldenhance the vortices intensity giving an added higher temperatures andpressure.

The said narrowing vortex cylinder-(G) 14 with its hot narrowing tubeoutlet with its adjustable hot outlet valve, this would give the neededadded higher pressure and temperature. Giving the said steam turbine-(M)24 the needed 500° C. (932° F.) steam temperature (500 kPa=72.5188Psi−up to 700 kPa=101.52642 Psi). Results in an increase of the twicemaximized cooling heat transfer rate of nearly 330% from 300 kPa to 700kPa. The said (G) 14 with its adjustable hot outlet valve temperatureand pressure output information is based on the publication of:Engenharia Termica (Thermal Engineering), Vol. 11 * No. 1-2 * June andDecember 2012-p. 85-92.

The water boils at 100° C. at the standard temperature and pressure. Thesaid narrowing vortex cylinder-(G) 14 with its outer hot end would beusing its air-radiation heat and the warm water lying within the saidradiation steam line-(L) 22. The said (G) 14 outer hot end would bereleasing its air-radiation heat energy to heat the water, to have awarm-water-to-hot-water-to-steam conversion. The said (G) 14, its innercold end would be releasing its cold air to cool the water, to have asteam-to-hot-to-warm water conversion.

The flash thermostatic valve-(T) 32 with its diverter valve, thediverter valve would divert the flash steam from the said return waterline-(P) 28 to via the flash steam line-chamber-(V) 34 to be cooled bythe cool air within the said flash steam cooling air chamber-(K) 20. Thesaid (K) 20 with its hot/warm water within, the hot/warm water would bepumped by the flash water pump-(W) 36. The said (W) 36 would pump thishot-warm water to via the said return water line-(P) 28 toward the saidwarm water pump-(R) 30.

The air-radiation heat would transfer to the warm water to make a steamconversion are well known. The cold air would lie within the said coldair cooling chamber-(J) 18. The steam and the hot water heat transfer tothe cold air also are well known. The Ranque-Hilsch vortex tube and thesteam turbines are well known. The said narrowing vortex cylinder-(G) 14is similar to and with many characterize of the Uni-flow vortex tube.The said steam turbine-(M) 24 is similar to and with many characterizeof other steam turbines.

PRIOR ART—CROSS REFERENCE RELATED APPLICATIONS

-   Schefler device (U.S. Pat. No. 746,388 issued December 1903)    Patented a: Steam turbine, known as “radial” in which steam reacts    on a plurality of turbine-wheels.-   Smith device (U.S. Pat. No. 777,313 issued December 1904) Patented    a: Steam turbine, relates to steam-turbines provided with curved    buckets.-   Ranque device (U.S. Pat. No. 1,952,281 issued March 1934) Patented    a: Vortex tube, also known as; the Ranque-Hilsch vortex tube (a    mechanical device that has no moving parts).-   Drier device (U.S. Pat. No. 1,961,179 issued May 1934) Patented a:    Electric drier (Relatively narrow annular slot of sufficient    diameter and inclined toward a focal point sufficiently forward of    the nozzle).-   S. De Lisio device (U.S. Pat. No. 2,488,467 issued November 1949)    Patented a: Motor-Driven Fan—An electric motor which drives a    blower, fan, impeller, or other having a suitable means, creating a    flow of air through the conduit and to and through the nozzles.-   Christopher device (U.S. Pat. No. 3,358,748 issued December 1967)    Patented a: A cooling systems of the kind including a direct contact    condenser, the condensate from which is fed to a cooler for cooling    by indirect heat exchange with air circulated over the cooler by a    dry cooling tower.-   Hogan device (U.S. Pat. No. 3,366,363 issued January 1968) Patented    a: A vent value to control the volume of flow there through and    moved therefrom.-   Inglis device (U.S. Pat. No. 4,240,261 issued December 1980)    Patented a: A vortex tube assembly equipped with a control mechanism    for use in selectively adjusting the temperature of air discharged    from the primary outlet of the assembly to any temperature within    the range from maximum hot to maximum cold.-   Yukl device (U.S. Pat. No. 4,494,009 issued January 1985) Patented    a: Method and apparatus for capturing an electrical potential    generated by a moving air mass.-   Dyson device (U.S. Pat. No. 4,593,429 issued June 1986) Patented a:    Vacuum cleaning appliance—A vacuum cleaning appliance with a cyclone    air unit.-   Lopez device (U.S. Pat. No. 4,594,084 issued June 1986) Patented a:    Air conditioning system. When the nozzles are of supersonic design,    they are capable of providing very high exits velocities, however,    these nozzles inherently are sensitive for off design conditions    such a pressure changes at the nozzle exits, etc. Therefore nozzles    that is slightly in the subsonic in design, “above Mach 0.9. The    design of these nozzles follows conventional design practices for    high efficiency ‘De Laval’ nozzles.-   Armbruster device (U.S. Pat. No. 4,856,968 issued August 1989)    Patented a: Air circulation device. The blade causes an axial flow    in relation to the rotational axis of the blades. Martin device    (U.S. Pat. No. 4,907,552 issued March 1990) Patented a: Forced air    induction system—Sucking-in of the air along an air flow path which    and is initiated by passing through.-   Kim device (U.S. Pat. No. 4,962,642 issued October 1990) Patented a:    Air flow system for an internal combustion engine. A swirling device    disposed therein having a plurality of vanes for causing the air to    swirl thereby improving the properties of the air-fuel mixture and    improving the performance of the engine.-   Michaud device (U.S. Pat. No. 7,086,823 issued August 2006) Patented    a: Atmospheric vortex engine. The vortex once established can be the    naturally occurring heat content of ambient air or can be provided    in a peripheral heat exchanger.-   Van Valkenburgh et al device (U.S. Application 2013/1401284 filed    August 2013) Patent application for a: Atmospheric Vortex Engine.    Filed an application for patent for a: Heating and refrigeration    apparatus. Using a plurality of high and low pressure region    increase the velocity air stream, to via the vortex generating zone.    The outer vortex and inner vortex functions by converting the water    molecules to absorb the latent heat.

BACKGROUND WITH ITS NEEDS

The apparatus-(A) 02 will have a much broader use by using anair-radiation heat transfer systems, as an alternative to theconventional fuel driven systems. The said (A) 02 is a non-pollutingenergy-efficient system. The said (A) 02 uses no fuel, like oil or gas,the only energy that being used is the electricity for the cylindermotor.

The apparatus-(A) 02 uses a two or a plurality of the narrowing spiraltube-(B) 04 with its vortex nozzle that would be connected with its oneof the two or a plurality of the narrowing volute generator-(C) 06 toproduce a high moving air stream medium for the narrowing vortexcylinder-(G) 14. There would be the same amount of numbers of the said(B) 04 with its vortex nozzle as there are in numbers of the said (C) 06with its vortex nozzle. The said (G) 14 with its vortex, the vortexwould have a temperatures separation effect. The vortex separated hightemperatures would produce the heat for the steam to be use by the steamturbine-(M) 24 producing torque for the drive shaft-(N) 26.

The Ranque-Hilsch vortex tube and the steam turbines are well known, asthese has many characterize with the narrowing vortex cylinder-(G) 14and with the steam turbine-(M) 24. The apparatus-(A) 02 is anenergy-efficient system, by using a low pressure ambient air to producea high moving air stream medium. The said (G) 14 would produce theair-radiation heat energy to generate the water conversion for theneeded steam to drive the said (M) 24 producing torque for the driveshaft-(N) 26.

The government regulations and consumer demands strongly encourage moreenergy-efficient fuel systems. Energy-efficient fuel systems are neededin: residential, commercial, industrial, automobiles, and watercraftsmotors. These systems are now being used, would generally be using arelatively high amount of energy. The apparatus-(A) 02 is useful for itsnon-polluting high energy-efficient system.

The United States emission standards and managed by the EnvironmentalProtection Agency (EPA) and California Air Resources Board wields anenormous influence over the emissions requirements, set specific limitsto the amount of pollution that can be released into the environment.America's has roughly 1,600 existing coal and gas-fired plants generateabout 40% of the country's carbon dioxide emissions. The apparatus-(A)02 is useful in cutting down on these carbon dioxide emissionsrequirements. Be useful in power stations, generating stations and orgenerating plants.

The United Nations' Intergovernmental Panel on climate Change says thatglobal warming is here, human-caused and probably already dangerous. Instudying the problems caused by the burning of fossil fuels, such ascoal, oil and gas paints a harsh warning of what's causing globalwarming. Continued emission of greenhouse gases will cause furtherwarming and long-lasting changes in all components of the climatesystem. Power plants account for roughly one-third of all U.S. emissionsof the heat-trapping gases blamed for global warming, making them thelargest single source. The apparatus-(A) 02 is useful in meeting theglobal warming requirements.

Research from NASA'S Goddard Space Flight Center shows that largequantities of a chemical responsible for depleting the ozone layer arestill being emitted, ever years after an international ban. Though theozone layer has seemed some recovery since the Montreal Protocol, theozone hole still persists today. The apparatus-(A) 02 is useful inmeeting these ozone requirements, by using non-polluting ambient airmedium for its energy needs.

The current torque driven systems utilize a considerable amount ofenergy. As oil or gas shortages have started to drive the fuel cost upthere is concern about the cost of running these current torque systems.The current torque systems need to be designed with considerations ofbeing low in polluting, with efficiency in mind, with an attempt toobtain more energetic systems. The apparatus-(A) 02 meets thisefficiency.

The apparatus-(A) 02 eliminate the problem of range anxiety associatedto all-electric vehicles. Other benefits include improved nationalenergy security, with the convenience of home recharging, opportunitiesto provide emergency backup power in the home, and vehicle-to grid (V2G)applications.

The apparatus-(A) 02 replaces a lot of the current high energetic mobiledriven systems with the said (A) 02 energy saving system. The said (A)02 is useful powertrain in versions for all kinds of vehicles, vans,trucks, buses, and watercrafts.

SUMMARY OF THE INVENTION

The apparatus-(A) 02 also would be known as the Vortex Turbine Engine;the present invention relates to an air driven and a steam drivensystem. The said (A) 02 will have a much broader use by using anair-radiation heat transfer systems, as an alternative to theconventional fuel driven systems. The said (A) 02 is a non-pollutingenergy-efficient system.

The said apparatus-(A) 02 is a closed area that would have an opening ateach one of the narrowing spiral tube-(B) 04 at its ambient air intakes,with an opening at the radiation boiler chamber-(H) 16 at its air heatoutlet, and with an opening at the flash steam cooling air chamber-(K)20 at its cold air outlet. The said (A) 02 is suitable as a one, two, ora plurality of units.

Of the main portion of the embodiments there will be only two movingsaid embodiments; that being the cyclone narrowing cylinder-(E) 10 thatbeing powered by the cylinder motor and the other one would be the steamturbine-(M) 24 producing torque for the drive shaft-(N) 26. The saidapparatus-(A) 02 uses no fuel, like oil or gas, the only energy thatbeing used is the electricity for the said cylinder motor. The said (A)02 uses no refrigerant of any kind to cool the air stream. With only aminimal of moving parts, this translates into virtually littlemaintenance.

The ambient air medium being drawn into each one of the said narrowingspiral tube-(B) 04 ambient air intakes, the air stream is being drawn inby the said cyclone narrowing cylinder-(E) 10 that being powered by thecylinder motor. The said (E) 10 converts the mechanical energy from thesaid cylinder motor, to energize the moving air stream.

The said apparatus-(A) 02 uses a two or a plurality of the saidnarrowing spiral tube-(8) 04 with its ingrained vortex nozzle, thesewould be connected to its one of the narrowing volute generator-(C) 06with its ingrained vortex nozzle, these would produce a high moving airstream medium from the said ambient air medium. There would be the sameamount of numbers of the said (B) 04 with its vortex nozzle as there arein numbers of the said (C) 06 with its vortex nozzle.

Each one of the said narrowing spiral tube-(B) 04 and along with eachone of the said narrowing volute generator-(C) 06, each one of thesewould have a converging portion that would have a greater diameter thanthe diverging portion, as these would enhance the vortices intensity.The drawing of the air causes a low pressure in front of the highpressured regions, causing the molecules to accelerate toward the lowpressure regions.

The said narrowing spiral tube-(B) 04 with its vortex nozzle with itsair stream, the air stream would via the said narrowing volutegenerator-(C) 06 with its vortex nozzle. The said (C) 06 with its vortexnozzle with its air stream, the air stream would via the fan chamber-(D)08. The said cyclone narrowing cylinder-(E) 10 joined to and would layin-between the said (D) 08 within its inner wall. The said (E) 10 spinon its horizontal-axis between the diameter interior side walls of thesaid (D) 08. The said (D) 08 bottom converging portion being round has agreater diameter than the top portion being round, to enhance its airstream intensity. The said (D) 08 with its air stream, the air streamwould via the said (E) 10.

The said cyclone narrowing cylinder-(E) 10 with its air stream now beingdriven by the said (E) 10 would via the advance narrowing chamber-(F)12. Each one of the said (F) 12 narrowing tube air outlets would beconnected to the narrowing vortex cylinder-(G) 14. The said (F) 12narrowing tube air outlets would enhance the vortices intensity withinthe said (G) 14.

The said narrowing vortex cylinder-(G) 14 would have a temperaturesseparation effect, separating its vortex intensity air stream into anair-radiation heat stream and a cold stream. The said (G) 14 with itsair-radiation heat, the air-radiation heat would via the said (G) 14that would have a hot narrowing tube outlet with adjustable hot outletvalve. The said (G) 14 having its adjustable hot outlet valve with itsair-radiation heat, the air-radiation heat would via the said radiationboiler chamber-(H) 16.

The radiation steam line-(L) 22 with its warm water, the warm waterwould absorb the latent heat lying within the said radiation boilerchamber-(H) 16 having an warm water-to-steam conversion. The said (L) 22with its warm water-to-steam conversion, the said steam would via thesaid steam turbine-(M) 24.

The said steam turbine-(M) 24 with its steam flow would generate arotating motion force, forcing the said drive shaft-(N) 26 to rotate onits horizontal-axis producing torque. The said (M) 24 with its hotsteam, the hot water of the steam would via the return water line-(P)28. The hot water coming from the said (M) 24, this hot water sometimeswould flash evaporation. The flash steam would via the flashthermostatic valve-(T) 32 with its diverter valve.

The said return water line-(P) 28 with its hot water, the hot water thatdid not flash evaporate to flash steam would via toward the warm waterpump-(R) 30. The said flash thermostatic valve-(T) 32 with its divertervalve, the diverter valve would divert the flash steam to via the flashsteam line-chamber-(V) 34. The said flash steam cooling air chamber-(K)20 with its cold air, the cold air stream would absorb the flash steamlatent heat that would be lying within the said (V) 34 having asteam-to-hot-warm water conversion.

The said flash steam line-chamber-(V) 34 with its steam-to-hot-warmwater conversion, the hot-warm water would via the flash water pump-(W)36. The said (W) 36 would pump this hot-warm water to via the saidreturn water line-(P) 28 toward the said warm water pump-(R) 30. Thesaid narrowing vortex cylinder-(G) 14 with its narrowing tube coldoutlet with its cold air, the cold air would via the cold air coolingchamber-(J) 18.

The said cold air cooling chamber-(J) 18 with its cold air, the cold airwould via the said flash steam cooling air chamber-(K) 20. The said (J)18 with its cold air stream, the cold air stream would absorb the latentheat from the hot water lying within the said return water line-(P) 28having a hot-to-warm water conversion.

The said return water line-(P) 28 with its hot-to-warm water conversion,the warm water would via the said warm water pump-(R) 30. The said (R)30 with its warm water, pumps the warm water to via the said radiationsteam line-(L) 22. The pumping causes a vacuum within the said (P) 28,drawing the said water toward the said (R) 30. The said (L) 22 with itswarm water-to-steam conversion therefore commence the warmwater-to-steam conversion cycle thereat.

SUMMARY Added Information: The Apparatus-NVCHACR-(NV) 02NV Systems.

A portion of the apparatus-(A) 02 is a non-vapor compression embodiment,this portion of the said (A) 02 would be known as; theapparatus-NVCHACR-(NV) 02NV (non-vapor compression, heating, cooling andrefrigeration) systems. The said (NV) 02NV is a non-vapor compressionthat uses no refrigerant. The said (NV) 02NV split-system with itstemperatures separation effect would be useful for its non-vaporcompression, heating and cooling and refrigeration systems.

The said split-system separate its cold temperatures (cold air stream)from its heat temperatures (air-radiation heat). The said cold airstream to via a cold air cooling chamber-(J) 18 and the saidair-radiation heat to via its adjustable hot outlet valve and then thesaid air-radiation heat would via the radiation boiler chamber-(H) 16.

The said apparatus-NVCHACR-(NV) 02NV comprises of: The narrowing spiraltube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D)08, the cyclone narrowing cylinder-(E) 10, the advance narrowingchamber-(F) 12, and the said narrowing vortex cylinder-(G) 14.

The said apparatus-NVCHACR-(NV) 02NV uses the said narrowing spiraltube-(B) 04, and the said narrowing volute generator-(C) 06, the saidfan chamber-(D) 08, the said cyclone narrowing cylinder-(E) 10, the saidadvance narrowing chamber-(F) 12, along with the said narrowing vortexcylinder-(G) 14. The said (G) 14 outer hot end would by releasing itsair-radiation heat would be used for the heating systems. The said (G)14 inner cold end would by releasing its cold air stream would be usedfor the cooling and refrigeration systems.

REFERENCE NUMBERS IN THE DRAWING AND WRITINGS

-   -   Vortex Turbine Engine: also known as; apparatus-(A) 02    -   02: apparatus-(A) 02: also known as; (A) 02    -   writings only: apparatus-NVCHACR-(NV) 02NV: also as; (NV) 02NV    -   04: narrowing spiral tube-(B) 04: also known as; (B) 04    -   06: narrowing volute generator-(C) 06: also known as; (C) 06    -   08: fan chamber-(D) 08: also known as; (D) 08    -   10: cyclone narrowing cylinder-(E) 10: also known as; (E) 10    -   12: advance narrowing chamber-(F) 12: also known as: (F) 12    -   14: narrowing vortex cylinder-(G) 14: also known as; (G) 14    -   16: radiation boiler chamber-(H) 16: also known as; (H) 16    -   18: cold air cooling chamber-(J) 18: also known as; (J) 18    -   20: flash steam cooling air chamber-(K) 20: also known as; (K)        20    -   22: radiation steam line-(L) 22: also known as; (L) 22    -   24: steam turbine-(M) 24: also known as; (M) 24    -   26: drive shaft-(N) 26: also known as; (N) 26    -   28: return water line-(P) 28: also known as; (P) 28    -   30: warm water pump-(R) 30: also known as; (R) 30    -   32: flash thermostatic valve-(T) 32: also known as; (T) 32    -   34: flash steam line-chamber-(V) 34: also known as; (V) 34    -   36: flash water pump-(W) 36: also known as; (W) 36

BRIEF DESCRIPTION OF THE DRAWING

The embodiments will now be described with reference to the accompanyingdrawing, wherein like reference numbers designate corresponding oridentical elements throughout the various drawing. The drawingsdescribed herein are for illustration possible only and are not intendedto limit the scope of the present disclosure in any way.

FIG. 1 is a perspective view of a cross-sectional of the apparatus-(A)02. The system constructed according to the principled of the said (A)02.

EMBODIMENT: COLD AIR AND AIR-RADIATION HEAT

The embodiments will now be described with reference to the accompanyingdrawing, wherein like reference numbers designate corresponding oridentical elements throughout the drawing. The Vortex Turbine Enginealso would be known as the apparatus-(A) 02. The said (A) 02 uses theapparatus-NVCHACR-(NV) 02NV for its split-system with its temperaturesseparation effect system.

The said apparatus-NVCHACR-(NV) 02NV comprises of: The narrowing spiraltube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D)08, the cyclone narrowing cylinder-(E) 10, the advance narrowingchamber-(F) 12, and the narrowing vortex cylinder-(G) 14.

The ambient air medium being drawn into each one of the said narrowingspiral tube-(B) 04 ambient air intakes, the air stream is being drawn inby the said cyclone narrowing cylinder-(E) 10. The said (B) 04 ambientair intake with its ambient air stream, the forward circumventing airstream would via the said (B) 04. The said (B) 04 with its air stream,the air stream would via its vortex nozzle.

The said narrowing spiral tube-(B) 04 vortex nozzle with its air stream,the circumventing air stream would via its one of the said narrowingvolute generator-(C) 06. The said (C) 06 with its forward circumventingair stream, the air stream would via its vortex nozzle. The said (C) 06vortex nozzle with its moving air stream, the air stream would via thesaid fan chamber-(D) 08.

The said cyclone narrowing cylinder-(E) 10 joined to and would layin-between the said fan chamber-(D) 08 within its inner wall. The said(D) 08 bottom converging portion being round has a greater diameter thanthe top portion being round, to enhance its air stream intensity. Thesaid (E) 10 spin on its horizontal-axis between the diameter interiorside walls of the said (D) 08. The said (D) 08 with its air stream, theair stream would via the said (E) 10. The said narrowing spiral tube-(B)04 ambient air intake, the said air stream is being drawn in by the said(E) 10 that being powered by the cylinder motor.

The air stream after being drawn in by the said cyclone narrowingcylinder-(E) 10, the air stream is then driven by the said (E) 10. Thesaid (E) 10 with its driven air stream, the air stream would via thesaid advance narrowing chamber-(F) 12. The said (F) 12 with its airstream, the air stream would via its said narrowing tube air outlets.

Each one of the said advance narrowing chamber-(F) 12 narrowing tube airoutlets with its air stream, the air stream would via the said narrowingvortex cylinder-(G) 14. The said (G) 14 having its temperatures, itstemperatures would have a separation effect within its vortex. The said(G) 14, its vortex outer air-radiation heat temperature would separatefrom its inner cold air.

The said narrowing vortex cylinder-(G) 14 with its temperaturesseparation effect would have the said vortex with an outer hot endreleasing its air-radiation heat. The said (G) 14 with an outer hot endreleasing its air-radiation heat to via the air-radiation heat would viaits hot narrowing tube outlet and would then via its adjustable hotoutlet valve. The said (G) 14 having its adjustable hot outlet valvewith its air-radiation heat, the air-radiation heat would via theradiation boiler chamber-(H) 16.

The said narrowing vortex cylinder-(G) 14 with its temperaturesseparation effect would have the said vortex with an inner cold endreleasing its cold air. The said (G) 14 with an inner cold end releasingits cold to via the said (G) 14 with its narrowing tube cold outlet withits cold air, the cold air would via the cold air cooling chamber-(J)18.

The radiation steam line-(L) 22 with its warm water, the warm waterwould absorb the air-radiation latent heat lying within the saidradiation boiler chamber-(H) 16. The said air-radiation heat would belying within the said (H) 16. The said warm water conversion to streamwould be lying within the said (L) 22. The said (L) 22 would have a warmwater-to-steam conversion. The said (H) 16 with its air-radiation heat,the air-radiation heat would via it's the said (H) 16 air heat outlet.

The said radiation boiler chamber-(H) 16 with its air heat outlet withits air-radiation heat, the now cooler air-radiation heat would exit thesaid apparatus-(A) 02. The return water line-(P) 28 would be lyingwithin the said cold air cooling chamber-(J) 18. The said (J) 18 withits cold air, the cold air stream would absorb the hot-warm water latentheat lying within the said (P) 28.

The said cold air would be lying within the said cold air coolingchamber-(J) 18. The said hot water would be lying within the said returnwater line-(P) 28. The said (P) 28 would have a hot-to-warm waterconversion. The said (J) 18 with its cold air stream, the cold airstream would via the flash steam cooling air chamber-(K) 20. The flashsteam line-chamber-(V) 34 would be lying within the said (K) 20.

The said flash steam cooling air chamber-(K) 20 with its warm-cold air,the warm-cold air stream would absorb the flash steam latent heat lyingwithin the said flash steam line-chamber-(V) 34. The said cold air wouldbe lying within the said (K) 20. The said flash steam heat would belying within the said (V) 34. The said (V) 34 would have asteam-to-hot-warm water conversion. The said (K) 20 with its warm-coldair, the warm-cold air would via its cold air outlet, and then thewarm-cold air stream would exit the said apparatus-(A) 02.

Embodiment: Water and Steam

The embodiments will now be described with reference to the accompanyingdrawing, wherein like reference numbers designate corresponding oridentical elements throughout the drawing.

The Vortex Turbine Engine also would be known as the apparatus-(A) 02.The water and steam embodiments portion of the said (A) 02 comprises of:The radiation boiler chamber-(H) 16, the cold air cooling chamber-(J)18, the flash steam cooling air chamber-(K) 20, the radiation steamline-(L) 22, the steam turbine-(M) 24, the drive shaft-(N) 26, thereturn water line-(P) 28, the warm water pump-(R) 30, the flashthermostatic valve-(T) 32, the flash steam line-chamber-(V) 34, theflash water pump-(W) 36.

The said radiation steam line-(L) 22 would be lying within the saidradiation boiler chamber-(H) 16. The said air-radiation heat would belying within the said (H) 16. The said warm water conversion to streamwould be lying within the said (L) 22. The said flash steamline-chamber-(V) 34 would be lying within the said flash steam coolingair chamber-(K) 20. The said cold air would be lying within the said (K)20.

The said flash steam heat to hot water would be lying within the saidflash steam line-chamber-(V) 34. The said return water line-(P) 28 wouldbe lying within the said cold air cooling chamber-(J) 18. The said coldair would be lying within the said (J) 18. The said hot water to warmwater would be lying within the said (P) 28.

The said warm water pump-(R) 30 with its warm water, pumps the warmwater to via the said radiation steam line-(L) 22. The said (L) 22 withits warm water, the warm water would absorb the latent heat lying withinthe said radiation boiler chamber-(H) 16. The said (L) 22 would have awarm water-to-steam conversion. The said (L) 22 with its warmwater-to-steam conversion, the steam would via the said steamturbine-(M) 24.

The said steam turbine-(M) 24 with its steam flow would generate arotating motion force, forcing the said drive shaft-(N) 26 to rotate onits horizontal-axis producing torque. The said (N) 26 would be joinedto, being part of the said (M) 24. The said (M) 24 would have a steamturning back to hot water conversion. The said (M) 24 with its hotsteam, the hot water of the steam would via the said return waterline-(P) 28.

The hot water coming from the said steam turbine-(M) 24, this hot watersometimes would flash evaporation within the said return water line-(P)28. The said flash steam within the said (P) 28 with its flash steam,the flash steam would via the said flash thermostatic valve-(T) 32 withits diverter valve. The said (P) 28 with its hot water, the hot waterthat did not flash to flash steam would via toward the said warm waterpump-(R) 30.

The said flash thermostatic valve-(T) 32 with its diverter valve, thediverter valve would divert the flash steam to via the said flash steamline-chamber-(V) 34. The flash steam that would flash evaporation isreleased by the said (T) 32 with its diverter valve. The said (T) 32with its diverter valve with its flash steam, the flash steam would viathe said (V) 34.

The said flash steam cooling air chamber-(K) 20 with its cold air, thecold air stream would absorb the flash steam latent heat lying withinthe said flash steam line-chamber-(V) 34. The said (V) 34 would have asteam-to-hot-warm water conversion. The said (V) 34 with itssteam-to-hot-warm water conversion, the hot-warm water would via thesaid flash water pump-(W) 36. The said (W) 36 with its hot-warm water,pumps the hot-warm water to via the said return water line-(P) 28.

The said flash water pump-(W) 36 would pump this hot-warm water to viathe said return water line-(P) 28. The said (P) 28 with its hot water,the water that did not flash to flash steam would via toward the said(R) 30. The said (W) 36 with its hot-warm water, this hot-warm waterbeing pump into the said (P) 28 would be pump toward the said (R) 30.The said cold air cooling chamber-(J) 18 with its cold air stream, thecold air stream would absorb the latent heat from the hot water lyingwithin the said (P) 28.

The said return water line-(P) 28 would have a hot water-to-warm waterconversion. The said (P) 28 with its hot-to-warm water conversion, thewarm water would via the said warm water pump-(R) 30. The said (R) 30with its warm water, pumps the warm water to via the said radiationsteam line-(L) 22. The said (L) 22 with its warm water-to-steamconversion therefore commence the warm water-to-steam conversion cyclethereat.

Embodiment

The embodiments will now be described with reference to the accompanyingdrawing, wherein like reference numbers designate corresponding oridentical elements throughout the drawing. The Vortex Turbine Enginealso would be known as the apparatus-(A) 02.

The apparatus-(A) 02 comprises of: The apparatus-NVCHACR-(NV) 02NV, theradiation boiler chamber-(H) 16, the cold air cooling chamber-(J) 18,the flash steam cooling air chamber-(K) 20, the radiation steam line-(L)22, the steam turbine-(M) 24, the drive shaft-(N) 26, the return waterline-(P) 28, the warm water pump-(R) 30, the flash thermostaticvalve-(T) 32, the flash steam line-chamber-(V) 34, the flash waterpump-(W) 36.

The apparatus-NVCHACR-(NV) 02NV comprises of: The narrowing spiraltube-(B) 04, the narrowing volute generator-(C) 06, the fan chamber-(D)08, the cyclone narrowing cylinder-(E) 10, the advance narrowingchamber-(F) 12, and the narrowing vortex cylinder-(G) 14. The said (NV)02NV embodiment portion would be a closed area that would have anopening at each one of the said narrowing spiral tube-(B) 04 at itsambient air intakes, the said narrowing vortex cylinder-(G) 14 at itsnarrowing tube cold outlet, and the said (G) 14 at its adjustable hotoutlet valve.

The apparatus-(A) 02: The said (A) 02 is suitable as a one, two, or aplurality of units. The said (A) 02 is a closed area that would have anopening at each one of the narrowing spiral tube-(B) 04 at its ambientair intakes, the radiation boiler chamber-(H) 16 at its air heat outlet,and the flash steam cooling air chamber-(K) 20 at its cold air outlet.

The narrowing spiral tube-(B) 04: The apparatus-(A) 02 would contain twoor a plurality of the said (B) 04 with each one with an ambient airintake and an ingrained vortex nozzle. There would be the same amount ofnumbers of the said (B) 04 with its vortex nozzle as there are innumbers of the narrowing volute generator-(C) 06 with its vortex nozzle.

The narrowing spiral tube-(B) 04: The ambient air medium being drawninto each one of the said (B) 04 ambient air intakes, the air stream isbeing drawn in by the cyclone narrowing cylinder-(E) 10. Each one of thesaid (B) 04 ambient air intakes is set at an angle to advance, generate,forming a vortex within each one of its one of the said (B) 04. Each oneof the said (B) 04 contains a vortex.

The narrowing spiral tube-(B) 04: The air stream gains velocity whilecircumventing into the said (B) 04 through its ambient air intake and isdrawn circumventing through the said (B) 04 and through its vortexnozzle. Each one of the said (B) 04 vortex nozzle is set at an angle toadvance, generate, forming a vortex within each one of it's one of thenarrowing volute generator-(C) 06.

The narrowing spiral tube-(B) 04: Each one of the said (B) 04 convergingportion has a greater diameter than the diverging portion, to enhancethe vortices intensity. Each one of the said (B) 04 converging portionhas a greater diameter than the diverging portion, to enhance thevortices intensity within each one of it's one of the narrowing volutegenerator-(C) 06. The said (B) 04 with its air stream, the air streamwould via its said vortex nozzle. Each one of the said (B) 04 vortexnozzle with its air stream, the air stream would via it's one of thesaid (C) 06.

The narrowing volute generator-(C) 06: Each one of the narrowing spiraltube-(B) 04 vortex nozzle with its air stream, the air stream would viait's one of the said (C) 06. The apparatus-(A) 02 would contain two or aplurality of the said (C) 06 with each one with an ingrained vortexnozzle. There would be the same amount of numbers of the said (C) 06with its vortex nozzle as there are in numbers of the said (B) 04 withits vortex nozzle. Each one of the said (C) 06 converging portion has agreater diameter than the diverging portion, to enhance its vorticesintensity. Each one of the said (C) 06 contains a vortex.

The narrowing volute generator-(C) 06: The air stream is drawncircumventing into the said (C) 06 and through its vortex nozzle. Thesaid (C) 06 air stream gains velocity while circumventing, being drawnthrough the said (C) 06 and through its vortex nozzle. Each one of thesaid (C) 06 vortex nozzle with its air stream, the air stream would viathe fan chamber-(D) 08.

The fan chamber-(D) 08: Each one of the narrowing volute generator-(C)06 vortex nozzle with its air stream, the air stream would via the said(D) 08. The said (D) 08 is connected to the advance narrowingchamber-(F) 12. The cyclone narrowing cylinder-(E) 10 joined to andwould lay in-between the said (D) 08 within its inner wall. The said (E)10 spin on its horizontal-axis between the diameter interior side wallsof the said (D) 08. The said (D) 08 bottom converging portion beinground has a greater diameter than the top portion being round, toenhance its air stream intensity. The said (D) 08 with its air stream,the air stream would via the said (E) 10.

The cyclone narrowing cylinder-(E) 10: The said (E) 10 converts themechanical energy from the cylinder motor, to energize the moving airstream. The energy of the said cylinder motor would energize the said(E) 10 through its rotating movement. The said (E) 10 air holes wouldenergize its rotating movement with an angle to capture the kineticenergy. The said (E) 10 joined to and would lay in-between the fanchamber-(D) 08 within its inner wall. The said (E) 10 spin on itshorizontal-axis between the diameter interior side walls of the said (D)08. The said (E) 10 would be joined to at the bottom of the said (D) 08.

The cyclone narrowing cylinder-(E) 10: The fan chamber-(D) 08 with itsair stream, the air stream would via the said (E) 10. The ambient airmedium being drawn into each one of the narrowing spiral tube-(B) 04ambient air intakes, the air stream is being drawn in by the said (E)10. The air stream is then driven by the said (E) 10. The said (E) 10converging portion would have a greater diameter than the divergingportion, to enhance the air flow intensity within the advance narrowingchamber-(F) 12. The said (E) 10 with its forward driven air stream, theair stream would via the said (F) 12.

The advance narrowing chamber-(F) 12: The cyclone narrowing cylinder-(E)10 with its forward driven air stream, the air stream would via the said(F) 12. The said (F) 12 converging portion has a greater diameter thanthe diverging portion, to enhance the air flow intensity within each oneof its narrowing tube air outlets. The said (F) 12 would contain two ora plurality of its narrowing tube air outlets.

The advance narrowing chamber-(F) 12: Each one of the said (F) 12narrowing tube air outlets converging portion would have a greaterdiameter than the diverging portion, to enhance the vortices intensitywithin the narrowing vortex cylinder-(G) 14. Each one of the said (F) 12narrowing tube air outlets would be connected to the said (G) 14. Eachone of the said (F) 12 narrowing tube air outlets contains a vortex. Thefan chamber-(D) 08 is connected to the said (F) 12.

The advance narrowing chamber-(F) 12: The said (F) 12 with its airstream would be driven by the cyclone narrowing cylinder-(E) 10. Thesaid (F) 12 with its air stream, the air stream would via it's the said(F) 12 narrowing tube air outlets. Each one of the said (F) 12 narrowingtube air outlets is set at an angle to advance, generate, and helps toform a vortex within the narrowing vortex cylinder-(G) 14. Each one ofthe said (F) 12 narrowing tube air outlets with its air stream, the airstream would via the said (G) 14.

The narrowing vortex cylinder-(G) 14: Each one of the advance narrowingchamber-(F) 12 narrowing tube air outlets with its air stream, the airstream would via the said (G) 14. The said (G) 14 would separate itscompressed vortex air stream into an air-radiation heat stream and acold stream. The said (G) 14 converging portion would have a greaterdiameter than the diverging portion, to enhance the vortices intensity,along with its air-radiation heat intensity of the vortex. The said (G)14 contains a vortex.

The narrowing vortex cylinder-(G) 14: The said (G) 14 having itstemperatures, its temperatures would have a separation effect within itsvortex. The said (G) 14, its vortex outer air-radiation heat temperaturewould separate from its inner cold air. The said (G) 14 with itstemperatures separation effect would have the said vortex with an outerhot end releasing its air-radiation heat. The said (G) 14 with itstemperatures separation effect, this would have its vortex with an innercold end releasing its cold air.

The narrowing vortex cylinder-(G) 14: The said (G) 14 would have an hotnarrowing tube outlet at the outer top end of the said (G) 14. The said(G) 14 hot narrowing tube outlet converging portion would have a greaterdiameter than the diverging portion, to enhance the air-radiation heatintensity. The said (G) 14 hot narrowing tube outlet would have anadjustable hot outlet valve at the outer top end of the said (G) 14 toadjust its air-radiation heat outward flow.

The narrowing vortex cylinder-(G) 14: The said (G) 14 with an outer hotend releasing its air-radiation heat, the air-radiation heat would viaits hot narrowing tube outlet and would then via its adjustable hotoutlet valve. The said (G) 14 having its adjustable hot outlet valvewith its air-radiation heat, the air-radiation heat would via theradiation boiler chamber-(H) 16.

The narrowing vortex cylinder-(G) 14: The said (G) 14 would have annarrowing tube cold outlet near the outer top end of the said (G) 14.The said (G) 14 would have narrowing tube cold outlet with itsadjustable hot outlet valve. The said (G) 14 with an inner cold endreleasing its cold air, the cold air would via it's the said (G) 14narrowing tube cold outlet. The said (G) 14 with its narrowing tube coldoutlet with its cold air, the cold air would via the cold air coolingchamber-(J) 18.

The radiation boiler chamber-(H) 16: The narrowing vortex cylinder-(G)14 having its adjustable hot outlet valve with its air-radiation heat,the air-radiation heat would via the said (H) 16. The radiation steamline-(L) 22 would be lying within the said (H) 16. The said (L) 22 withits warm water, the warm water would absorb the latent heat lying withinthe said (H) 16. The said air-radiation heat would be lying within thesaid (H) 16. The said warm water conversion to stream would be lyingwithin the said (L) 22. The said (L) 22 would have a warm water-to-steamconversion.

The radiation boiler chamber-(H) 16: The said (H) 16 with itsair-radiation heat within, the air-radiation heat would via its air heatoutlet. The said (H) 16 with its air heat outlet with its air-radiationheat, the now cooler air-radiation heat would exit the apparatus-(A) 02.

The cold air cooling chamber-(J) 18: The narrowing vortex cylinder-(G)14 with its narrowing tube cold outlet with its cold air, the cold airwould via the said (J) 18. The return water line-(P) 28 would be lyingwithin the said (J) 18. The said (J) 18 with its cold air stream, thecold air stream would absorb the latent heat from the hot water lyingwithin the said (P) 28. The said cold air would be lying within the said(J) 18. The said hot water would be lying within the said (P) 28. Thesaid (P) 28 would have a hot-to-warm water conversion. The said (J) 18with its cold air, the cold air would via the flash steam cooling airchamber-(K) 20.

The flash steam cooling air chamber-(K) 20: The cold air coolingchamber-(J) 18 with its cold air, the cold air would via the said (K)20. The flash steam line-chamber-(V) 34 would be lying within the said(K) 20. The said (K) 20 with its cold air, the cold air stream wouldabsorb the flash steam latent heat lying within the said (V) 34. Thesaid cold air would be lying within the said (K) 20. The said flashsteam heat would be lying within the said (V) 34. The said (V) 34 wouldhave a steam-to-hot-warm water conversion. The said (K) 20 with itscold-warm air, the cold-warm air would via its cold air outlet. The said(K) 20 with its cold air outlet with its cold-warm air, the cold-warmair would exit the apparatus-(A) 02.

The radiation steam line-(L) 22: The warm water pump-(R) 30 with itswarm water, pumps the warm water to via the said (L) 22. The said (L) 22would be lying within the radiation boiler chamber-(H) 16. The said (L)22 with its warm water, the warm water would absorb the latent heatlying within the said (H) 16. The said air-radiation heat would be lyingwithin the said (H) 16. The said warm water conversion to stream wouldbe lying within the said (L) 22. The said (L) 22 would have a warmwater-to-steam conversion. The said (L) 22 with its warm water-to-steamconversion, the steam would via the steam turbine-(M) 24.

The steam turbine-(M) 24: The radiation steam line-(L) 22 with its warmwater-to-steam conversion, the steam would via the said (M) 24. The said(M) 24 with its steam flow would generate a rotating motion force,forcing the drive shaft-(N) 26 to rotate on its horizontal-axisproducing torque. The said (N) 26 would be joined to, being part of thesaid (M) 24. The said (M) 24 would have a steam turning back to hotwater conversion. The said (M) 24 with its hot steam, the hot water ofthe steam would via the return water line-(P) 28.

The drive shaft-(N) 26: The steam turbine-(M) 24 with its steam flowwould generate a rotating motion force, forcing the said (N) 26 torotate on its horizontal-axis producing torque. The said (N) 26 would bejoined to, being part of the said (M) 24.

The return water line-(P) 28: The steam turbine-(M) 24 with its hotsteam, the hot water of the steam would via the said (P) 28. The hotwater coming from the said (M) 24, this hot water sometimes would flashevaporation (also known as flash steam). The said (P) 28 with its flashsteam, the flash steam would via the flash thermostatic valve-(T) 32with its diverter valve. The said (P) 28 with its hot water, the hotwater that did not flash evaporate to flash steam would via toward thewarm water pump-(R) 30.

The flash thermostatic valve-(T) 32: The return water line-(P) 28 withits flash steam, the flash steam would via the said (T) 32 with itsdiverter valve. The said (T) 32 with its diverter valve, the divertervalve would divert the flash steam to via the flash steamline-chamber-(V) 34. The flash steam that would flash evaporation isreleased by the said (T) 32 with its diverter valve. The said (T) 32diverter valve with its flash steam, the flash steam would via the said(V) 34.

The flash steam line-chamber-(V) 34: The flash thermostatic valve-(T) 32diverter valve with its flash steam, the flash steam would via the said(V) 34. The flash steam cooling air chamber-(K) 20 would be lying withinthe said (V) 34. The said (K) 20 with its cold air, the cold air streamwould absorb the flash steam latent heat lying within the said (V) 34.

The flash steam line-chamber-(V) 34: The said cold air would be lyingwithin the flash steam cooling air chamber-(K) 20. The said flash steamheat would be lying within the said (V) 34. The said (V) 34 would have asteam-to-hot-warm water conversion. The said (V) 34 with itssteam-to-hot-warm water conversion, the hot-warm water would via theflash water pump-(W) 36.

The flash water pump-(W) 36: The flash steam line-chamber-(V) 34 withits steam-to-hot-warm water conversion, the hot-warm water would via thesaid (W) 36. The said (W) 36 with its hot-warm water, pumps the hot-warmwater to via the return water line-(P) 28. The said (W) 36 would pumpthis hot-warm water to via the said (P) 28 toward the warm waterpump-(R) 30.

The return water line-(P) 28: The flash water pump-(W) 36 with itshot-warm water, pumps the hot-warm water to via the said (P) 28. Thesaid (P) 28 with its hot water, the water that did not flash to flashsteam lying within the said (P) 28 would via toward the warm waterpump-(R) 30. The said (P) 28 would be lying within the cold air coolingchamber-(J) 18.

The return water line-(P) 28: The cold air cooling chamber-(J) 18 withits cold air stream, the cold air stream would absorb the latent heatfrom the hot water lying within the said (P) 28. The said cold air wouldbe lying within the said (J) 18. The said hot water would be lyingwithin the said (P) 28. The said (P) 28 would have a hot-to-warm waterconversion. The said (P) 28 with its hot-to-warm water conversion, thewarm water would via the warm water pump-(R) 30.

The warm water pump-(R) 30: The return water line-(P) 28 with its hotwater-to-warm water, the warm water would via toward the said (R) 30.The said (R) 30 with its warm water, pumps the warm water to via theradiation steam line-(L) 22. The pumping causes a vacuum within the said(P) 28, drawing the said water toward the said (R) 30. The said (L) 22with its warm water-to-steam conversion therefore commence the warmwater-to-steam conversion cycle thereat.

Embodiment: Non-Vapor Compression NVCHACR-(NV) 02NV Systems

The apparatus-NVCHACR-(NV) 02NV: A portion of the apparatus-(A) 02 is anon-vapor compression. This portion of the said (A) 02 would be knownas; the said (NV) 02NV (non-vapor compression, heating, cooling andrefrigeration). The said (NV) 02NV with its temperatures separationeffect, separating its cold air from its latent heat is an embodimentportion of the said (A) 02. The said (NV) 02NV systems, is the systemsbeing used in the said (A) 02 to heat and cool its air stream. The said(NV) 02NV is a non-vapor compression that uses no refrigerant.

The apparatus-NVCHACR-(NV) 02NV: The said (NV) 02NV systems embodimentportion would be a closed area that would have an opening at each one ofthe narrowing spiral tube-(B) 04 at its ambient air intakes, thenarrowing vortex cylinder-(G) 14 at its narrowing tube cold outlet, andthe said (G) 14 at its adjustable hot outlet valve. The said (NV) 02NVwould contain two or a plurality of the said (B) 04 with each one withan ambient air intake and an ingrained vortex nozzle. The ambient airmedium being drawn into each one of the said (B) 04 ambient air intakes,the air stream is being drawn in by the cyclone narrowing cylinder-(E)10.

The narrowing spiral tube-(B) 04: Each one of the said (B) 04 ambientair intakes is set at an angle to advance, generate, forming a vortexwithin each one of its one of the said (B) 04. Each one of the said (B)04 contains a vortex. The air stream gains velocity while circumventinginto the said (B) 04 through its ambient air intake and is drawncircumventing through the said (B) 04 and through its vortex nozzle.Each one of the said (B) 04 vortex nozzle is set at an angle to advance,generate, forming a vortex within each one of it's one of the narrowingvolute generator-(C) 06.

The narrowing spiral tube-(B) 04: Each one of the said (B) 04 convergingportion has a greater diameter than the diverging portion, to enhancethe vortices intensity. Each one of the said (B) 04 converging portionhas a greater diameter than the diverging portion, to enhance thevortices intensity within each one of it's one of the narrowing volutegenerator-(C) 06. The said (B) 04 with its air stream, the air streamwould via its said vortex nozzle. Each one of the said (B) 04 vortexnozzle with its air stream, the air stream would via within each of itsown one of the said (C) 06. There would be the same amount of numbers ofthe said (B) 04 with its vortex nozzle as there are in numbers of thesaid (C) 06 with its vortex nozzle.

The narrowing volute generator-(C) 06: Each one of the narrowing spiraltube-(B) 04 vortex nozzle with its air stream, the air stream would viait's one of the said (C) 06. The apparatus-NVCHACR-(NV) 02NV wouldcontain two or a plurality of the said (C) 06 with each one with aningrained vortex nozzle. There would be the same amount of numbers ofthe said (C) 06 with its vortex nozzle as there are in numbers of thesaid (B) 04 with its vortex nozzle. Each one of the said (C) 06converging portion has a greater diameter than the diverging portion, toenhance its vortices intensity.

The narrowing volute generator-(C) 06: Each one of the said (C) 06contains a vortex. The air stream is drawn circumventing into the said(C) 06 and through its vortex nozzle. The said (C) 06 air stream gainsvelocity while circumventing, being drawn through the said (C) 06 andthrough its vortex nozzle. Each one of the said (C) 06 vortex nozzlewith its air stream, the air stream would via the fan chamber-(D) 08.

The fan chamber-(D) 08: Each one of the narrowing volute generator-(C)06 vortex nozzle with its air stream, the air stream would via the said(D) 08. The said (D) 08 is connected to the advance narrowingchamber-(F) 12. The cyclone narrowing cylinder-(E) 10 joined to andwould lay in-between the said (D) 08 within its inner wall. The said (E)10 spin on its horizontal-axis between the diameter interior side wallsof the said (D) 08. The said (D) 08 bottom converging portion beinground has a greater diameter than the top portion being round, toenhance its air stream intensity.

The cyclone narrowing cylinder-(E) 10: The said (E) 10 converts themechanical energy from the cylinder motor, to energize the moving airstream. The energy of the said cylinder motor would energize the said(E) 10 through its rotating movement. The said (E) 10 air holes wouldenergize its rotating movement with an angle to capture the kineticenergy. The said (E) 10 joined to and would lay in-between the fanchamber-(D) 08 within its inner wall. The said (E) 10 spin on itshorizontal-axis between the diameter interior side walls of the said (D)08. The said (E) 10 would be joined to at the bottom of the said (D) 08.

The cyclone narrowing cylinder-(E) 10: The fan chamber-(D) 08 with itsair stream, the air stream would via the said (E) 10. The ambient airmedium being drawn into each one of the narrowing spiral tube-(B) 04ambient air intakes, the air stream is being drawn in by the said (E)10. The air stream is then driven by the said (E) 10. The said (E) 10converging portion would have a greater diameter than the divergingportion, to enhance the air flow intensity within the advance narrowingchamber-(F) 12. The said (E) 10 with its forward driven air stream, theair stream would via the said (F) 12.

The advance narrowing chamber-(F) 12: The cyclone narrowing cylinder-(E)10 with its forward driven air stream, the air stream would via the said(F) 12. The said (F) 12 converging portion has a greater diameter thanthe diverging portion, to enhance the air flow intensity within each oneof its narrowing tube air outlets. The said (F) 12 would contain two ora plurality of its narrowing tube air outlets.

The advance narrowing chamber-(F) 12: Each one of the said (F) 12narrowing tube air outlets converging portion would have a greaterdiameter than the diverging portion, to enhance the vortices intensitywithin the narrowing vortex cylinder-(G) 14. Each one of the said (F) 12narrowing tube air outlets would be connected to the said (G) 14. Eachone of the said (F) 12 narrowing tube air outlets contains a vortex. Thefan chamber-(D) 08 is connected to the said (F) 12.

The advance narrowing chamber-(F) 12: The said (F) 12 with its airstream would be driven by the cyclone narrowing cylinder-(E) 10. Thesaid (F) 12 with its air stream, the air stream would via it's the said(F) 12 narrowing tube air outlets. Each one of the said (F) 12 narrowingtube air outlets is set at an angle to advance, generate, and helps toform a vortex within the narrowing vortex cylinder-(G) 14. Each one ofthe said (F) 12 narrowing tube air outlets with its air stream, the airstream would via the said (G) 14.

The narrowing vortex cylinder-(G) 14: Each one of the advance narrowingchamber-(F) 12 narrowing tube air outlets with its air stream, the airstream would via the said (G) 14. The said (G) 14 would separate itscompressed vortex air stream into an air-radiation heat stream and acold stream. The said (G) 14 converging portion would have a greaterdiameter than the diverging portion, to enhance the vortices intensity,along with its air-radiation heat intensity of the vortex. The said (G)14 contains a vortex.

The narrowing vortex cylinder-(G) 14: The said (G) 14 having itstemperatures, its temperatures would have a separation effect within itsvortex. The said (G) 14, its vortex outer air-radiation heat temperaturewould separate from its inner cold air. The said (G) 14 with itstemperatures separation effect would have the said vortex with an outerhot end releasing its air-radiation heat. The said (G) 14 with itstemperatures separation effect, this would have its vortex with an innercold end releasing its cold air.

The narrowing vortex cylinder-(G) 14: The said (G) 14 would have an hotnarrowing tube outlet at the outer top end of the said (G) 14. The said(G) 14 hot narrowing tube outlet converging portion would have a greaterdiameter than the diverging portion, to enhance the air-radiation heatintensity. The said (G) 14 hot narrowing tube outlet would have anadjustable hot outlet valve at the outer top end of the said (G) 14 toadjust its air-radiation heat outward flow.

The narrowing vortex cylinder-(G) 14: The said (G) 14 with an outer hotend releasing its air-radiation heat, the air-radiation heat would viaits hot narrowing tube outlet and would then via its adjustable hotoutlet valve. The said (G) 14 having its adjustable hot outlet valvewith its air-radiation heat, the air-radiation heat would exit theapparatus-NVCHACR-(NV) 02NV.

The narrowing vortex cylinder-(G) 14: The said (G) 14 would have annarrowing tube cold outlet near the outer top end of the said (G) 14.The said (G) 14 with an inner cold end releasing its cold air, the coldair would via it's the said (G) 14 narrowing tube cold outlet. The said(G) 14 with its narrowing tube cold outlet with its cold air, the coldair would exit the apparatus-NVCHACR-(NV) 02NV.

Embodiment: Information

Air induction: The air being drawn into the narrowing spiral tube-(B)04, causing an air pressure buildup on the atmospheric high pressureregions. The vacuum in the front of the molecules, in this high pressureregion causes the molecules (matter) to accelerate toward the lowpressure regions. Air induction is used within the said (B) 04 and thenthe air flow would via its one of the narrowing volute generator-(C) 06.

Atmospheric gases: The common name given to the atmospheric gases usedin breathing and photosynthesis is air. In a gas, the molecules haveenough energetic so that the effect of intermolecular forces is small,and the typical distance between neighboring molecules is much greaterthan the molecular size.

Atmospheric pressure: Is the force per unit area exerted on a surface bythe weight of air above that surface, the higher the atmosphericpressure, the higher the ambient air pressure buildup. The drawing ofthe ambient air pressure causes a vacuum in the high pressure regions.The vacuum in the front of the molecules causes the molecules toaccelerate toward the low pressure regions.

Atmospheric pressure: The apparatus-(A) 02 uses the atmospheric pressurehigh and low pressure regions. The cyclone narrowing cylinder-(E) 10draws the ambient air medium into the said (A) 02, through the narrowingspiral tube-(B) 04 ambient air intake, then through its ingrained vortexnozzle, the narrowing volute generator-(C) 06 with its ingrained vortexnozzle, then driven through the advance narrowing chamber-(F) 12, thesaid (F) 12 narrowing tube air outlets and the narrowing vortexcylinder-(G) 14. The drawing of its air from the high pressured regionscauses a vacuum in front of the high pressured regions. This cause avacuum (low pressure) in the atmospheric high pressure regions, thisvacuum in front of the high pressure causes the molecules to acceleratetoward the low pressure regions.

Bernoulli principle: The correlation between air speed and pressure, asspeed increases pressure decreases, as the air is curving. Thecontinuous change of position of a body of air stream curving within theapparatus-(A) 02, so that every partied of the body follows astraight-line path. The Bernoulli principle is used in the narrowingspiral tube-(B) 04 with its ingrained vortex nozzle, the narrowingvolute generator-(C) 06 with its ingrained vortex nozzle, the advancenarrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets andthe narrowing vortex cylinder-(G) 14.

Conservation laws, in physics: As air is drawn circumventing into thenarrowing spiral tube-(B) 04, the narrowing volute generator-(C) 06,then driven through the advance narrowing chamber-(F) 12 with itsnarrowing tube air outlets and the said (F) 12, and the said (F) 12narrowing tube air outlets, a corresponding volume must move a greaterdistance in their narrowing of the passageways and thus have a greaterspeed. At the same time, the work done by corresponding volumes in thenarrowing of the passageways will be expressed by the product of thepressure and the volume. Since the speed is greater in the narrowing ofthe passageways, the energetic of that volume is greater. Then, by thelaw of conservation of energy, this increase in kinetic energy must bebalanced by a decrease in the pressure-volume product, or, since thevolumes are equal, by a decrease in pressure.

Converging and diverging portions: Each one of these: The narrowingspiral tube-(B) 04 with its ingrained vortex nozzle, the narrowingvolute generator-(C) 06 with its ingrained vortex nozzle, the advancenarrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets andthe narrowing vortex cylinder-(G) 14, all of these has a converging anddiverging portion, to enhance the vortices intensity. The said (G) 14hot narrowing tube outlet would have a converging and diverging portion,to enhance the air-radiation heat temperature intensity. The convergingportion has a greater diameter than the diverging portion. Theconverging portion has a high capacity and a low velocity. The divergingportion will have a low capacity and a high velocity with a backpressure. The ambient pressure, referred to as lower atmosphericpressure, (back pressure) causes the air stream to accelerate. Byreducing the pressure of the air at the exit of the expansion portion,in effect, the molecules leave the outlets at their thermal speedwithout colliding with other molecules. This is because the moleculesare all moving in the same relative direction and at the same speed.

Diverter valve: The pressure is relieved by allowing the pressurizedsteam (flash evaporation) to flow from the return water line-(P) 28, thepressurized steam would via the diverter valve of the flash thermostaticvalve-(T) 32. The diverter valve is designed or set to open at apredetermined set pressure to protect the said (P) 28 and the otherequipment from being subjected to pressures that exceed their designlimits. The said (T) 32 control the volume and temperature, and by usinga diverter valve this would divert the steam that would be released bythe said (T) 32, this pressurized steam would via the flash steamline-chamber-(V) 34.

Flash steam: Is a name given to the steam formed from hot condensatewhen the pressure is reduced. Flash steam is no different from normalsteam. The hot water that is produced from the steam turbine-(M) 24,this hot water would via the return water line-(P) 28. Whereas flashsteam occurs when high pressure and high temperature condensate isexposed to a large pressure drop such as when being released by the said(M) 24 and would via the said (P) 28. High temperature condensatecontains high energy that cannot remain in liquid form at a lowerpressure because there is more energy than that required to achievesaturated water at the lower pressure. The result is that some of theexcess energy causes a % of the condensate to flash within the said (P)28.

Heat transfer: Describes the exchange of thermal energy, betweenphysical systems depending on the temperature and pressure, bydissipating heat. The fundamental modes of heat transfer are conductionor diffusion, convection and radiation. The exchange of kinetic energyof particles: Through the boundary between two systems at differenttemperatures, from each other from their surroundings. Heat transferalways occurs from a region of high temperature to another region oflower temperature. Heat transfer changes the internal energy of bothsystems involved according to the First Law of Thermodynamics. TheSecond Law of Thermodynamics defines the concept of thermodynamicentropy, by measurable heat transfer. The apparatus-(A) 02 uses its twosystems with the different temperatures. The narrowing vortexcylinder-(G) 14 would have a narrowing tube cold outlet, releasing itscold air. With the inner cold end, the flash steam line-chamber-(V) 34and the return water line-(P) 28 would have a hot to cold conversion.The said (G) 14 would have an adjustable hot outlet valve, releasing itsair-radiation heat. With the outer hot end, the radiation steam line-(L)22 would have a cold/warm to steam conversion.

Kinetic Molecular Theory of Matter: Is a concept that basically statesthat atoms and molecules possess energy of motion (kinetic energy) thatwe perceive as temperature. In other words, atoms and molecules areconstantly in motion, and we measure the energy of these movements asthe temperature of that substance. This means if there is an increase intemperature, the atoms and molecules will gain more energy (kineticenergy) and move even faster. The narrowing spiral tube-(B) 04, thenarrowing volute generator-(C) 06, the advance narrowing chamber-(F) 12,the said (F) 12 narrowing tube air outlets, the narrowing vortexcylinder-(G) 14; possesses energy of motion.

Kinetic momentum: The momentum which a particle possesses because of itsmotion, equal to the particle's mass times it velocity. The narrowingspiral tube-(B) 04, the narrowing volute generator-(C) 06, the advancenarrowing chamber-(F) 12, the said (F) 12 narrowing tube air outlets,the narrowing vortex cylinder-(G) 14 air outward motion mass, equaltimes it velocity. The rotational energetic depends on rotation about anaxis, and for a body of constant moment of inertia is equal to theproduct of half the moment of inertia times the square of the angularvelocity. In relativistic physics kinetic energy is equal to the productof the increase of mass caused by motion times the square of the speedof light.

Mach number=1: Assuming air to be an ideal gas, the formula to computeMach number in a subsonic compressible flow is found from Bernoulli'sequation for M<1.

Narrowing vortex cylinder-(G) 14: The said (G) 14 with a convergingportion that has a greater diameter than the diverging portion. The said(G) 14 consists of a high pressure circumventing air stream that entersthe said (G) 14 and the air-radiation heat passes through its said hotnarrowing tube outlet and then through it's said adjustable hot outletvalve. The gas expands through its said adjustable hot outlet valve andachieves a high angular velocity, causing a vortex-type flow. There aretwo exits to the said (G) 14: the said hot narrowing tube outlet thatthe air-radiation heat passing through and then through the saidadjustable hot outlet valve, that exit is placed near the outer radiusof the said (G) 14 at the end away from its said narrowing tube coldoutlet exit that is placed at the center of the said (G) 14 at the sameend as the said adjustable hot outlet valve. By adjusting its said hotnarrowing tube outlet with its said adjustable hot outlet valvedownstream of the said exit, it is possible to vary the fraction of theincoming air flow that leaves through it's said narrowing tube coldoutlet, referred as cold fraction. This adjustment affects the amount ofcold and hot energy that leaves the said (G) 14 through its exits.Results in an increase of the twice maximized cooling heat transfer rateof nearly 330% from 300 kPa to 700 kPa. (700 kPa=101.52642 Psi) The said(G) 14 with its said adjustable hot outlet valve temperature andpressure output information is based on the publication of: EngenhariaTermica (Thermal Engineering), Vol. 11 * No. 1-2 * June and December2012-p. 85-92.

Newton's first law of motion: Linear motion is the basic of all motion.According to Newton's first law of motion, objects that do notexperience any net force will continue to move in a straight line with aconstant velocity until they are subjected to a net force.

Pressure: Is a defined as the force per unit area exerted against asurface by the weight of the air above that surface. In terms ofmolecules, if the number of molecules above a surface increases, thereare more molecules to exert a force on that surface and consequently,the pressure increases.

Air-radiation heat transfer: Radiation is a method of heat transfer thatdoes not rely upon any contact between the heat source and the heatedobject as is the case with conduction and convection. Heat can betransmitted though empty space by thermal radiation is often calledinfrared radiation. The narrowing vortex cylinder-(G) 14 uses theair-radiation heat transfer. The transfer of the air-radiation heatcoming from the said (G) 14 this said air-radiation heat stream would betransferred through its adjustable hot outlet valve. With this transferof the said air-radiation heat, the radiation steam line-(L) 22 wouldhave a cold/warm water to steam conversion.

Ranque-Hilsch vortex tube: The vortex tube has been used for manydecades in various engineering applications. Because of its compactdesign and little maintenance requirements, it is very popular inheating and cooling processes. There is no unifying theory that explainsthe temperature separation phenomenon inside the vortex tube. The vortextube is a mechanical device that separates compressed air into anoutward radial high temperature region and an inner lower one. There aretwo classifications of the vortex tube. Both of these are currently inuse in the industry. The more popular is the counter-row vortex tube andthe Uni-flow vortex tube. The narrowing vortex cylinder-(G) 14 issimilar to with many characterize of the Uni-flow vortex tube.

Sound waves: In physics, sound is a vibration that propagates as atypically audible mechanical wave of pressure and displacement, througha medium such as air. In physiology and psychology, sound is thereception of such waves and their perception by the brain. Theapparatus-(A) 02 in accordance with its design has the means to adjustits outward air flow speed, therefore reducing its sound waves.

Steam: Is a term for the gaseous phase of water, which is formed whenwater boils. Technically speaking, in terms of the chemistry andphysics, steam is invisible and cannot be seen, however in commonlanguage it is often used to refer to the visible mist or aerosol ofwater droplets formed as this water vapor condenses in the presence of(cooler) air. At lower pressures, such as in the upper atmosphere or atthe top of high mountains water boils at a lower temperature than thenominal 100° C. (212° F.) at standard temperature and pressure. Today'svortex tube with its adjustable valve can reach temperatures as high as+200° C. and the air emerging from its inner cold end can reach −50° C.are possible. The narrowing vortex cylinder-(G) 14 would separate itsair stream into an air-radiation heat stream and a cold stream. The said(G) 14, the converging portion has a greater diameter than the divergingportion, to enhance the vortices intensity giving this an added highertemperatures along with its hot narrowing tube outlet with itsadjustable hot outlet valve. The steam turbine-(M) 24 needs 500° C.(932° F.) (500 kPa=72.5188 Psi) to produce its needed steam pressure.The said (G) 14 with its hot narrowing tube outlet and along with itsadjustable hot outlet valve giving the needed 500° C. (932° F.) (500kPa=72.5188 Psi) to produce its needed steam pressure. To increase ofthe twice maximized cooling heat transfer rate of nearly 330% from 300kPa to 700 kPa. (700 kPa=101.52642 Psi).

Steam turbine: There are two basic types of the steam turbines; bladesor the nozzles. Blades move entirely due to the impact of steam on themand their profiles do not converge. This results in a steam velocitydrop and essentially no pressure drop as steam moves through the blades.A turbine composed of blades alternating with fixed nozzles is called animpulse turbine, Curtis turbine, Rateau turbine, or Brown-Curtisturbine. Nozzles appear similar to blades, but their profiles convergenear the exit. This results in a steam pressure drop and velocityincrease as steam moves through the nozzles. Nozzles move due to boththe impact of steam on them and the reaction due to the high-velocitysteam at the exit. A turbine composed of moving nozzle alternating withfixed nozzles is called a reaction turbine or Parsons Turbine. The steamturbines are well known, as these has many characterize of the steamturbine-(M) 24.

Subsonic: As a gas is forced through a tube, the gas molecules aredeflected by the walls of the tube. If the speed of the gas is much lessthan the speed of sound of the gas, the density of the gas remainsconstant and the velocity of the flow increases. However, as the speedof the flow approaches the speed of sound we must considercompressibility effects on the gas. The density of the gas varies fromone location to the next. Considering flow through a tube, if the flowis very gradually compressed (area decreases) and then graduallyexpanded (area increases), the flow conditions return to their originalvalues. We say that such a process is reversible. From a considerationof the second law of thermodynamics, a reversible flow maintains aconstant value of entropy.

Vacuum: An approximation to such vacuum is a region with a gaseouspressure much less than atmospheric. This causes the circumventing airstream (molecule) to accelerate toward the low pressure regions. Theapparatus-(A) 02 uses these vacuums to move the air stream from highpressure regions to low pressure regions. The drawing of the air fromthe high pressured regions causes a vacuum in front of the highpressured regions. This causes a vacuum (low pressure) in theatmospheric high pressure region, with this vacuum in front of the highpressure causes the molecules would accelerate toward the low pressureregions. The narrowing spiral tube-(B) 04 along with the narrowingvolute generator-(C) 06, use this drawing of the ambient air medium,causing a vacuum (low pressure). The return water line-(P) 28 uses the(vacuum) low pressure regions to draw the flowing water toward the warmwater pump-(R) 30.

Vortex: The vortices are a measure of the intensity of a vortex. Animportant mechanism that enhances the vortices is the stretching of thevortex—stretching along the axis of the vortex, makes it rotate fasterand decreases its diameter in order to constantly maintain its kineticmomentum. The narrowing spiral tube-(B) 04, the narrowing volutegenerator-(C) 06, the advance narrowing chamber-(F) 12, the said (F) 12narrowing tube air outlets and the narrowing vortex cylinder-(G) 14 usesthis stretching to enhance the vortices intensity.

Vortex nozzle: The vortex nozzle is also call a CD-nozzle or aconvergent-divergent nozzle. The air enters the converging section, itsvelocity increases, considering the mass flow rate to be constant. Thegas passes through the throat, it attains sonic velocity (Machnumber=1). As the gas passes through the divergent section, the gaswould velocity to be supersonic (also Mach 1). The air speed would bekeep subsonic. The narrowing spiral tube-(B) 04 with its vortex nozzle,along with the narrowing volute generator-(C) 06 with its vortex nozzle,all of these would use its converging and divergent to increasevelocity.

Vortex tube: The water boils at 100° C. at the standard temperature andpressure. Today's vortex tube outer hot end can reach temperatures ashigh as +200° C. and the air emerging from its inner cold end can reach−50° C. are possible. The narrowing vortex cylinder-(G) 14 wouldseparate its compressed air into an air-radiation heat stream and a coldstream. Each one of the narrowing spiral tube-(B) 04 narrowingpassageways, along with each one of the narrowing volute generator-(C)06 narrowing passageways, the advance narrowing chamber-(F) 12 and thesaid (F) 12 narrowing tube air outlets, and along with the said (G) 14,all of these would have their converging portion would have a greaterdiameter than the diverging portion, to enhance the vortices intensitygiving an added higher temperatures and pressure. The said (G) 14 withits hot narrowing tube outlet and along with its adjustable hot outletvalve giving the needed 500° C. (932° F.) (500 kPa=72.5188 Psi) toproduce its needed steam pressure. The adjustable hot outlet valveincrease of the twice maximized cooling heat transfer rate of nearly330% from 300 kPa to 700 kPa. (700 kPa=101.52642 Psi).

Embodiment Communication, Connected, Ingrained, Joined, Means, Supports

Embodiment has the means to be attached, connected, continuous, joinedto or in transmission of something from one point to another point. Theapparatus-(A) 02 has the means to attach to and supports each one of thestructures of its embodiments. The said (A) 02 in communication withone, two, or with a plurality of units or an assembly of units. The said(A) 02 has the means to and would be in communication with eachembodiment. Each embodiment would be in communication with the said (A)02.

Each one of the narrowing spiral tube-(B) 04 would have an ambient airintake. Each one of the said (B) 04 with its ingrained vortex nozzle isconnected to it's one of the narrowing volute generator-(C) 06. Each oneof the said (C) 06 with its ingrained vortex nozzle is connected to thefan chamber-(D) 08.

The fan chamber-(D) 08 is connected to the advance narrowing chamber-(F)12. The said (D) 08 is joined to and would have the means to support thestructure of the cyclone narrowing cylinder-(E) 10. The said (E) 10would be joined to the cylinder with its motor shaft. The said (E) 10would be joined to and would lay in-between the said (D) 08 within itsinner wall. The cylinder motor with its drive shaft would be joined tothe said (E) 10. The said cylinder motor with its drive shaft would bejoined to and made part of the said cylinder motor. The said cylindermotor with its drive shaft would be not shown in the drawing.

Each one of the advance narrowing chamber-(F) 12 narrowing tube airoutlets is connected to the narrowing vortex cylinder-(G) 14. The said(G) 14 with its hot narrowing tube outlet with its adjustable hot outletvalve is connected to the radiation boiler chamber-(H) 16. The said (H)16 would have an air heat outlet, exiting the apparatus-(A) 02. The said(G) 14 with its narrowing tube cold outlet is connected to the cold aircooling chamber-(J) 18. The said (J) 18 is connected to the flash steamcooling air chamber-(K) 20. The said (K) 20 would have a cold airoutlet, exiting the said (A) 02.

The radiation steam line-(L) 22 is connected to the steam turbine-(M)24. The drive shaft-(N) 26 would be joined to, being part of the said(M) 24. The said (M) 24 is connected to the return water line-(P) 28.The said (P) 28 is connected to the flash thermostatic valve-(T) 32 withits diverter valve. The said (P) 28 is also connected to the warm waterpump-(R) 30. The said (P) 28 is also connected to the flash waterpump-(W) 36.

The flash thermostatic valve-(T) 32 with its diverter valve is connectedto the flash steam line-chamber-(V) 34. The said (V) 34 is connected tothe flash water pump-(W) 36. The said (W) 36 is connected to the returnwater line-(P) 28. The warm water pump-(R) 30 is connected to theradiation steam line-(L) 22.

Embodiment: Transfer to, Means to

Transfer to: The narrowing spiral tube-(B) 04, narrowing volutegenerator-(C) 06, fan chamber-(D) 08, cyclone narrowing cylinder-(E) 10,the advance narrowing chamber-(F) 12, the said (F) 12 narrowing tube airoutlets, narrowing vortex cylinder-(G) 14, the said (G) 14 narrowingtube cold outlet, the said (G) 14 hot narrowing tube outlet or being hotnarrowing tube outlets, the radiation boiler chamber-(H) 16, the coldair cooling chamber-(J) 18, and the flash steam cooling air chamber-(K)20, are compartment, tube or pipe with the means to transfer the airstream and or the air-radiation heat from one point to the next point.

Transfer to: The radiation steam line-(L) 22, return water line-(P) 28,flash steam line-chamber-(V) 34 are compartment, tube or pipe with themeans to transfer the steam and or the hot-warm water from one point tothe next point. The warm water pump-(R) 30 and along with the flashwater pump-(W) 36 with the means to transfer the hot-warm water orcold/warm water from one point to the next point.

Means to: The apparatus-(A) 02 to have means to start, stop, and controlor adjust the cylinder motor to rotate or to spin the cyclone narrowingcylinder-(E) 10 on its horizontal-axis shaft. The said (E) 10 would bejoined within and at the bottom end of the fan chamber-(D) 08, with themeans to rotate on its horizontal-axis. The said (E) 10 utilizes thesaid cylinder motor with the means to start, stop, and control or adjustits rotating or spinning within the said (D) 08. The said cylinder motorhas the means to force the said (E) 10 on its horizontal-axis shaft torotate or to spin.

Means to: The apparatus-(A) 02 to have means to start, stop, andcontrol, adjust the warm water pump-(R) 30, the flash water pump-(W) 36,and the flash thermostatic valve-(T) 32 with its diverter valve. Asensor with the means to adjust and control the water level that beingrelease by the said (R) 30. The radiation steam line-(L) 22, the returnwater line-(P) 28, and the flash steam line-chamber-(V) 34 would havethe means, to adjust and/or control the water level or its watertemperature.

Means to: The narrowing vortex cylinder-(G) 14 hot narrowing tube outletwith its adjustable hot outlet valve has the means to adjust, thisadjustment to have the effects of the amount of cold and hot energy thatleaves the said (G) 14 through its exits. The said (G) 14 hot narrowingtube outlet with an adjustable hot outlet valve built into the outer hotend releasing its air-radiation heat.

Embodiment: Hydrophilic Polymers Grafting Treatment

The hydrophilic polymers: The hydrophilic polymers grafting treatmentalong walls that are exposed to water as needed: The radiation steamline-(L) 22, the steam turbine-(M) 24, the return water line-(P) 28, thewarm water pump-(R) 30, the diverter valve of the flash thermostaticvalve-(T) 32, the flash steam line-chamber-(V) 34, and the flash waterpump-(W) 36, with the option to use, have, or be grafted along any orany other areas, where treatment is needed.

HydroLAST™: HydroLAST™ is a process by which hydrophilic polymers aregrafted permanently to the surface of a hydrophobic substrate. Thehydrophilic polymer has carboxyl, hydroxil, or amine functionalitiesthat serve to loosely bind water. Once treated, the substrate “wets out”and allows water and reagents to flow easily over or through it (in thecase of porous substrates). Unlike conventional hydrophilic treatmentssuch as straight plasma, corona, or ozone processing, the surface ispermanently rather than transiently hydrophilic.

Embodiment: Alternative Embodiment

Any such methods are natural outgrowths of the system or apparatusclaims. Natural outgrowths, alternative embodiment are not shown in thedrawing.

The apparatus-(A) 02 alternative: The said (A) 02 would have analternative to use only one and not the other one: the two or aplurality of the narrowing spiral tube-(B) 04 with its ingrained vortexnozzle or to use the two or a plurality of the narrowing volutegenerator-(C) 06 with its ingrained vortex nozzle. Each one of the said(B) 04 narrowing passageways or the said (C) 06 narrowing passageways;being used with its vortex nozzle would be connected to the fanchamber-(D) 08.

The apparatus-(A) 02 alternative: The said (A) 02 would have analternative to use one, two or a plurality of additional cylinders andjoined to their motor or motors. The said additional cylinders would bein front of and near or joined to the narrowing spiral tube-(B) 04ambient air intakes, driving the ambient air medium into each one of thesaid ambient air intakes. The said alternative would be used to keep theair pressure moving through the said (B) 04 ambient air intakes and thenthrough the said (B) 04 narrowing passageways. The said (B) 04additional cylinder being used would be in unison with the drawing ofthe air stream of the cyclone narrowing cylinder-(E) 10 through the said(B) 04 narrowing passageways.

The narrowing spiral tube-(B) 04 alternative: The said (B) 04 would havean alternative with the means to open, close, partial open or adjust itsangle on the said (B) 04 vortex nozzle, and or to use other kinds ofnarrowing passageways or nozzles.

The narrowing vortex cylinder-(G) 14 alternative: The said (G) 14narrowing tube cold outlet would have an alternative to have anadjustable cold outlet valve near the inner top end of the said (G) 14to adjust its cold air outward flow.

The radiation boiler chamber-(H) 16 alternative: The said (H) 16 wouldhave the alternative with a sensor to adjust the amount of air-radiationheat, flowing through the said (H) 16. The said (H) 16 would have analternative to use a release valve, adjusting the amount air-radiationheat, exiting the apparatus-(A) 02.

The cold air cooling chamber-(J) 18 alternative: The said (J) 18 wouldhave the alternative with sensors to adjust the amount of cold air,flowing through the said (J) 18. The said (J) 18 would have alternativerelease outlet, to adjust it measurement of flow out, to be able torelease its adjusted amount of cold air being released to exit theapparatus-(A) 02.

The steam turbine-(M) 24 alternative: The said (M) 24 would have thealternative of using any one of these different possible uses or useother different possible uses. The said (M) 24 turbine blades are of twobasic types, blades and nozzles. Blades move entirely due to the impactof steam on them and their profiles do not converge. This results in asteam velocity drop and essentially no pressure drop as steam movesthrough the blades. A turbine composed of blades alternating with fixednozzles is called an impulse turbine, Curtis turbine, Rateau turbine, orBrown-Curtis turbine. Nozzles appear similar to blades, but theirprofiles converge near the exit. This results in a steam pressure dropand velocity increase as steam moves through the nozzles. Nozzles movedue to both the impact of steam on them and the reaction due to thehigh-velocity steam at the exit. A turbine composed of moving nozzlesalternating with fixed nozzles is called a reaction turbine or ParsonsTurbine.

The return water line-(P) 28 alternative: The said (P) 28 would have thealternative to be fitted with an check valve to prevent a waterback-flow and alternative be fitted with an control valve to control itswater level. The said sensor with the alternative would be to adjust andcontrol the water temperature being release by the warm water pump-(R)30.

The flash steam line-chamber-(V) 34 alternative: The said (V) 34 wouldhave the alternative to use an added or an back up flash thermostaticvalve-(T) 32 with an diverter valve, to divert and release its flashsteam to exit the apparatus-(A) 02 if needed.

DETAILED DESCRIPTION Vortex Turbine Engine

In describing a preferred embodiment of the invention illustrated in thedrawings, specific terminology will be resorted to for the sake ofclarity. However, the invention is not intended to be limited to thespecific terms so selected, and it is to be understood that eachspecific term includes all technical equivalents which operate in asimilar manner to accomplish a similar purpose.

The present description provides for the Vortex Turbine Engine alsowould be known as the apparatus-(A) 02: The said (A) 02 is a closed areathat would have an opening at each one of the narrowing spiral tube-(B)04 at its ambient air intakes, the radiation boiler chamber-(H) 16 atits air heat outlet, and the flash steam cooling air chamber-(K) 20 atits cold air outlet.

The said apparatus-(A) 02 comprises of the apparatus-NVCHACR-(NV) 02NV,the said radiation boiler chamber-(H) 16, the cold air coolingchamber-(J) 18, the said flash steam cooling air chamber-(K) 20, theradiation steam line-(L) 22, the steam turbine-(M) 24, the driveshaft-(N) 26, the return water line-(P) 28, the warm water pump-(R) 30,the flash thermostatic valve-(T) 32, the flash steam line-chamber-(V)34, the flash water pump-(W) 36. The said (NV) 02NV comprises of: Thesaid narrowing spiral tube-(B) 04, the narrowing volute generator-(C)06, the fan chamber-(D) 08, the cyclone narrowing cylinder-(E) 10, theadvance narrowing chamber-(F) 12, the narrowing vortex cylinder-(G) 14.

The said apparatus-NVCHACR-(NV) 02NV embodiment portion would be aclosed area that would have an opening at each one of the said narrowingspiral tube-(B) 04 at its ambient air intakes, the said narrowing vortexcylinder-(G) 14 at its narrowing tube cold outlet, and the said (G) 14at its adjustable hot outlet valve.

The said apparatus-(A) 02 would contain two or a plurality of the saidnarrowing spiral tube-(B) 04 with each one with an ambient air intakeand an ingrained vortex nozzle. Each one of the said (B) 04 ambient airintakes is set at an angle to advance, generate, forming a vortex withineach one of its one of the said (B) 04. The ambient air medium beingdrawn into each one of the said (B) 04 ambient air intakes, the airstream is being drawn in by the said cyclone narrowing cylinder-(E) 10.

Each one of the said narrowing spiral tube-(B) 04 converging portion hasa greater diameter than the diverging portion, to enhance the vorticesintensity. Each one of the said (B) 04 converging portion has a greaterdiameter than the diverging portion, to enhance the vortices intensitywithin each one of it's one of the said narrowing volute generator-(C)06.

Each one of the said narrowing spiral tube-(B) 04 contains a vortex.Each one of the said (B) 04 vortex nozzle is set at an angle to advance,generate, forming a vortex within each one of its one of the saidnarrowing volute generator-(C) 06. The said (B) 04 with its air stream,the air stream would via its said vortex nozzle. Each one of the said(B) 04 vortex nozzle with its air stream, the air stream would via it'sone of the said (C) 06.

The said apparatus-(A) 02 would contain two or a plurality of the saidnarrowing volute generator-(C) 06 with each one with an ingrained vortexnozzle. There would be the same amount of numbers of the said narrowingspiral tube-(B) 04 with its vortex nozzle as there are in numbers of thesaid narrowing volute generator-(C) 06 with its vortex nozzle. Each oneof the said (C) 06 converging portion has a greater diameter than thediverging portion, to enhance its vortices intensity. Each one of thesaid (C) 06 contains a vortex.

The air stream is drawn circumventing into the said narrowing volutegenerator-(C) 06 and through its vortex nozzle. The said (C) 06 airstream gains velocity while circumventing, being drawn through the said(C) 06 and through its vortex nozzle. Each one of the said (C) 06 vortexnozzle with its air stream, the air stream would via the said fanchamber-(D) 08.

The said fan chamber-(D) 08 is connected to the said advance narrowingchamber-(F) 12. The said cyclone narrowing cylinder-(E) 10 joined to andwould lay in-between the said (D) 08 within its inner wall. The said (E)10 spin on its horizontal-axis between the diameter interior side wallsof the said (D) 08. The said (D) 08 bottom converging portion beinground has a greater diameter than the top portion being round, toenhance its air stream intensity. The said (D) 08 with its air stream,the air stream would via the said (E) 10.

The said cyclone narrowing cylinder-(E) 10 converts the mechanicalenergy from the cylinder motor, to energize the moving air stream. Theenergy of the said cylinder motor would energize the said (E) 10 throughits rotating movement. The said (E) 10 air holes would energize itsrotating movement with an angle to capture the kinetic energy. The said(E) 10 would be joined to and would lay in-between the said fanchamber-(D) 08 within its inner wall. The said (E) 10 would be joined toat the bottom of the said (D) 08.

The ambient air medium being drawn into each one of the said narrowingspiral tube-(B) 04 ambient air intakes, the air stream is being drawn inby the said cyclone narrowing cylinder-(E) 10. The air stream is thendriven by the said (E) 10. The said (E) 10 converging portion would havea greater diameter than the diverging portion, to enhance the air flowintensity within the said advance narrowing chamber-(F) 12. The said (E)10 with its forward driven air stream, the air stream would via the said(F) 12.

The said advance narrowing chamber-(F) 12 converging portion has agreater diameter than the diverging portion, to enhance the air flowintensity within each one of its narrowing tube air outlets. The said(F) 12 would contain two or a plurality of its narrowing tube airoutlets. Each one of the said (F) 12 narrowing tube air outletsconverging portion would have a greater diameter than the divergingportion, to enhance the vortices intensity within the said narrowingvortex cylinder-(G) 14.

Each one of the said advance narrowing chamber-(F) 12 narrowing tube airoutlets would be connected to the said narrowing vortex cylinder-(G) 14.Each one of the said (F) 12 narrowing tube air outlets contains avortex. The said fan chamber-(D) 08 is connected to the said (F) 12. Thesaid (F) 12 with its air stream would be driven by the said cyclonenarrowing cylinder-(E) 10.

The said advance narrowing chamber-(F) 12 with its air stream, the airstream would via its said narrowing tube air outlets. Each one of thesaid (F) 12 narrowing tube air outlets is set at an angle to advance,generate, and helps to form a vortex within the said narrowing vortexcylinder-(G) 14. Each one of the said (F) 12 narrowing tube air outletswith its air stream, the air stream would via the said (G) 14.

The said narrowing vortex cylinder-(G) 14 would separate its compressedair into an air-radiation heat stream and a cold stream. The said (G) 14converging portion would have a greater diameter than the divergingportion, to enhance the vortices intensity, along with its air-radiationheat intensity of the vortex. The said (G) 14 contains a vortex.

The said narrowing vortex cylinder-(G) 14 having its temperatures, itstemperatures would have a separation effect within its vortex. The said(G) 14, its vortex outer air-radiation heat temperature would separatefrom its inner cold air. The said (G) 14 with its temperaturesseparation effect would have the said vortex with an outer hot endreleasing its air-radiation heat. The said (G) 14 with its temperaturesseparation effect would have its vortex with an inner cold end releasingits cold air.

The said narrowing vortex cylinder-(G) 14 would have an hot narrowingtube outlet at the outer top end of the said (G) 14. The said (G) 14 hotnarrowing tube outlet converging portion would have a greater diameterthan the diverging portion, to enhance the air-radiation heat intensity.The said (G) 14 hot narrowing tube outlet would have an adjustable hotoutlet valve at the outer top end of the said (G) 14 to adjust itsair-radiation heat outward flow.

The said narrowing vortex cylinder-(G) 14 with an outer hot endreleasing its air-radiation heat, the air-radiation heat would via itshot narrowing tube outlet and would then via its adjustable hot outletvalve. The said (G) 14 having its adjustable hot outlet valve with itsair-radiation heat, the air-radiation heat would via the said radiationboiler chamber-(H) 16.

The said narrowing vortex cylinder-(G) 14 would have an narrowing tubecold outlet near the outer top end of the said (G) 14. The said (G) 14narrowing tube cold outlet be near the inner top end of the said (G) 14.The said (G) 14 with an inner cold end releasing its cold air, the coldair would via it's the said (G) 14 narrowing tube cold outlet. The said(G) 14 with its narrowing tube cold outlet, with its cold air, the coldair would via the said cold air cooling chamber-(J) 18.

The said air-radiation heat would be lying within the said radiationboiler chamber-(H) 16. The said radiation steam line-(L) 22 would belying within the said (H) 16. The said (L) 22 with its warm water, thewarm water would absorb the latent heat lying within the said (H) 16.The said warm water conversion to stream would be lying within the said(L) 22. The said (L) 22 would have a warm water-to-steam conversion. Thesaid (H) 16 with its air-radiation heat within, the air-radiation heatwould via its air heat outlet. The said (H) 16 with its air heat outletwith its air-radiation heat, the now cooler air-radiation heat wouldexit the said apparatus-(A) 02.

The said cold air cooling chamber-(J) 18 with its cold air stream, thecold air stream would absorb the latent heat from the hot water lyingwithin the said return water line-(P) 28. The said (P) 28 would be lyingwithin the said (J) 18. The said cold air would be lying within the said(J) 18. The said hot water would be lying within the said (P) 28. Thesaid (P) 28 would have a hot-to-warm water conversion. The said (J) 18with its cold air, the cold air would via the said flash steam coolingair chamber-(K) 20.

The said flash steam cooling air chamber-(K) 20 with its cold air, thecold air stream would absorb the flash steam latent heat lying withinthe said flash steam line-chamber-(V) 34. The said (V) 34 would be lyingwithin the said (K) 20. The said cold air would be lying within the said(K) 20. Said flash steam heat would be lying within the said (V) 34. Thesaid (V) 34 would have a steam-to-hot-warm water conversion. The said(K) 20 with its cold-warm air, the cold-warm air would via its cold airoutlet. The said (K) 20 with its cold air outlet with its cold-warm air,the cold-warm air would exit the said apparatus-(A) 02.

The said warm water pump-(R) 30 with its warm water, pumps the warmwater to via the said radiation steam line-(L) 22. The said (L) 22 withits warm water-to-steam conversion, the steam would via the said steamturbine-(M) 24. The said (M) 24 with its steam flow would generate arotating motion force, forcing the said drive shaft-(N) 26 to rotate onits horizontal-axis producing torque.

The said drive shaft-(N) 26 would be joined to, being part of the saidsteam turbine-(M) 24. The said (M) 24 would have a steam turning back tohot water conversion. The said (M) 24 with its hot steam, the hot waterof the steam would via the said return water line-(P) 28. The hot watercoming from the said (M) 24, this hot water sometimes would flashevaporation (also known as flash steam).

The said return water line-(P) 28 with its flash steam, the flash steamwould via the said flash thermostatic valve-(T) 32 with its divertervalve. The said (P) 28 with its hot water, the hot water that did notflash evaporate to flash steam would via toward the said warm waterpump-(R) 30.

The said flash thermostatic valve-(T) 32 with its diverter valve, thediverter valve would divert the flash steam to via the said flash steamline-chamber-(V) 34. The said flash steam that would flash evaporationis released by the said (T) 32 with its diverter valve. The said (T) 32diverter valve with its flash steam, the flash steam would via the said(V) 34.

The said flash steam line-chamber-(V) 34 with its steam-to-hot-warmwater conversion, the hot-warm water would via the said flash waterpump-(W) 36. The said (V) 34 with its steam-to-hot-warm waterconversion, the hot-warm water would via the said (W) 36. The said (W)36 with its hot-warm water, pumps the hot-warm water to via the saidreturn water line-(P) 28. The said (W) 36 would pump this hot-warm waterto via the said (P) 28 toward the said warm water pump-(R) 30.

The said return water line-(P) 28 with its hot water, the water that didnot flash to flash steam lying within the said (P) 28 would via towardthe said warm water pump-(R) 30. The said (P) 28 with its hot-to-warmwater conversion, the warm water would via the said (R) 30.

The said warm water pump-(R) 30 with its warm water, pumps the warmwater to via the said radiation steam line-(L) 22. The pumping causes avacuum within the said return water line-(P) 28, drawing the said watertoward the said (R) 30. The said (L) 22 with its warm water-to-steamconversion therefore commence the warm water-to-steam conversion cyclethereat.

Embodiment: In Many Different Forms

While the invention is susceptible to embodiment in many differentforms, as shown in the drawings and will be described to herein indetail, specific embodiments thereof with the understanding that thepresent disclosure is to be considered as an exemplification of theprinciples of the invention and is not to be limited to the specificembodiments described.

Each example is provided by way of explanation of the invention, notlimitation of the invention. In fact, it will be apparent to thoseskilled in the art that various modifications and variations can be madein the present invention without departing from the scope or spirit ofthe invention.

For instance, features illustrated or described as component of oneembodiment can be used with another embodiment to yield a still furtherembodiment.

Thus, it is intended that the present invention covers such modificationand variations as come within the scope of the appended claims and theirequivalents. It should be appreciated that the present invention is notlimited to any particular type or style depicted in Figure's and is forillustrative purposes only.

Ramifications of Detailed Description

Although preferred embodiments have been depicted and described indetail therein, it will be apparent to those skilled in the relevant artthat various modifications, additions, substitutions and the like can bemade without departing from the spirit of the invention and these aretherefore considered to be within the scope of the invention as definedin the following claims. All water temperatures, pressurized steam, airtemperatures, air velocity or air pressures used are an estimate, basedon information attained.

One of these changes could be without departing from essence presentinvention, by having other kinds of air moving devices, such as usingother kinds of engines, motors or multi-speed turbo fan motors to pulland drive the air stream into and through the apparatus. Having themotor placed in other locations, on, within or outside of the apparatus.Having the apparatus to use other kinds of, air blower holes or blades.There being other kinds of means to drive the apparatus other thanelectrically. Other kinds of power sources, like using solar energy. Useisolation material and formulation to reduce vibrations and dissipateshock energy for the motor and air mover.

Other change could be having the air intakes or air outlets, placedhigher or lower, smaller or larger, more or less of them on theapparatus. There being other kinds of tubes or piping, or more vortexesor other kinds of on-off switches, nozzles, controllers, rate adjustersor other kinds of adjuster.

It is not practical to describe in claims all possible embodiments,Embodiments may be accomplished generally in keeping with presentinvention. Disclosure may include, separately or collectively, aspectsdescribed found throughout description of patent. While these may beadded to explicitly include such details. Existing claims shouldconstrue to encompass such aspects.

To the extent methods claimed in present invention are not furtherdiscussed. Any such methods are natural outgrowths of the system orapparatus claims.

Therefore, separate and further discussions of the methods are deemedunnecessary. Otherwise claim steps implicit in use and manufacture orsystems or apparatus claims.

Furthermore, steps organized in logical fashion and other sequences canand do occur. Therefore, method claims should not be construed toinclude only this order. Other order and sequence steps may bepresented.

Notice: Subject to any disclaimer, the term of patent is extended oradjusted under 35 U.S.C. 154(b) by 501 days.

It is to be understood that the present invention is not limited to theembodiments described above, but encompasses any and all embodimentswithin the following scope of the following claims.

1. An apparatus-(A) accelerate air stream to form and producing an fastmoving vortex air producing to have an temperatures separation effecthaving its air-radiation heat separate from its air stream producing theseparated high temperatures that would produce an water-to-steamconversion and using this steam would be used in the steam turbine-(M)producing torque; the said apparatus-(A) is a closed area with anopening at each one of the narrowing spiral tube-(B) at its ambient airintakes and the radiation boiler chamber-(H) at its air heat outlet andthe flash steam cooling air chamber-(K) at its cold air outlet; the saidapparatus-(A) comprises of the apparatus-NVCHACR-(NV) of the saidradiation boiler chamber-(H) and the cold air cooling chamber-(J) andthe said flash steam cooling air chamber-(K) and the radiation steamline-(L) and the said steam turbine-(M) and the drive shaft-(N) and thereturn water line-(P) and the warm water pump-(R) and the flashthermostatic valve-(T) and the flash steam line-chamber-(V) and theflash water pump-(W); the said apparatus-NVCHACR-(NV) comprises of thesaid narrowing spiral tube-(B) and the narrowing volute generator-(C)and the fan chamber-(D) and the cyclone narrowing cylinder-(E) and theadvance narrowing chamber-(F) and the narrowing vortex cylinder-(G); thesaid apparatus-NVCHACR-(NV) embodiment portion would be a closed areathat would have an opening at each one of the said narrowing spiraltube-(B) at its ambient air intakes and the said narrowing vortexcylinder-(G) at its narrowing tube cold outlet and the said narrowingvortex cylinder-(G) at its adjustable hot outlet valve; the saidapparatus-(A) would contain two or a plurality of the said narrowingspiral tube-(B) with each one with an ambient air intake and aningrained vortex nozzle and each one of the said narrowing spiraltube-(B) ambient air intakes is set at an angle to advance and generateand that would be forming a vortex within each one of its one of thesaid narrowing spiral tube-(B); the ambient air medium being drawn intoeach one of the said narrowing spiral tube-(B) ambient air intakes andthe air stream is being drawn in by the said cyclone narrowingcylinder-(E); each one of the said narrowing spiral tube-(B) convergingportion has a greater diameter than the diverging portion that is toenhance the vortices intensity; each one of the said narrowing spiraltube-(B) converging portion has a greater diameter than the divergingportion that is to enhance the vortices intensity within each one ofit's one of the said narrowing volute generator-(C); each one of thesaid narrowing spiral tube-(B) contains a vortex; each one of the saidnarrowing spiral tube-(B) vortex nozzle is set at an angle to advanceand generate and to forming a vortex within each one of its one of thesaid narrowing volute generator-(C); the said narrowing spiral tube-(B)with its air stream and the air stream would via its said vortex nozzle;each one of the said narrowing spiral tube-(B) vortex nozzle with itsair stream and the air stream would via it's one of the said narrowingvolute generator-(C); the said apparatus-(A) would contain two or aplurality of the said narrowing volute generator-(C) with each one withan ingrained vortex nozzle; there would be the same amount of numbers ofthe said narrowing spiral tube-(B) with its vortex nozzle as there arein numbers of the said narrowing volute generator-(C) with its vortexnozzle; each one of the said narrowing volute generator-(C) convergingportion has a greater diameter than the diverging portion that is toenhance its vortices intensity; each one of the said narrowing volutegenerator-(C) contains a vortex; the air stream is drawn circumventinginto the said narrowing volute generator-(C) and through its vortexnozzle; the said narrowing volute generator-(C) air stream gainsvelocity while circumventing that is being drawn through the saidnarrowing volute generator-(C) and through its vortex nozzle; each oneof the said narrowing volute generator-(C) vortex nozzle with its airstream and the air stream would via the said fan chamber-(D); the saidfan chamber-(D) is connected to the said advance narrowing chamber-(F);the said cyclone narrowing cylinder-(E) joined to and would layin-between the said fan chamber-(D) within its inner wall; the saidcyclone narrowing cylinder-(E) spin on its horizontal-axis between thediameter interior side walls of the said fan chamber-(D); the said fanchamber-(D) bottom converging portion being round has a greater diameterthan the top portion being round as this would enhance its air streamintensity; the said fan chamber-(D) with its air stream and the airstream would via the said cyclone narrowing cylinder-(E); the saidcyclone narrowing cylinder-(E) converts the mechanical energy from thecylinder motor that would energize the moving air stream; the energy ofthe said cylinder motor would energize the said cyclone narrowingcylinder-(E) through its rotating movement; the said cyclone narrowingcylinder-(E) air holes would energize its rotating movement with anangle to capture the kinetic energy; the said cyclone narrowingcylinder-(E) would be joined to and would lay in-between the said fanchamber-(D) within its inner wall; the said cyclone narrowingcylinder-(E) would be joined to at the bottom of the said fanchamber-(D); the ambient air medium being drawn into each one of thesaid narrowing spiral tube-(B) ambient air intakes and the air stream isbeing drawn in by the said cyclone narrowing cylinder-(E) the air streamis then driven by the said cyclone narrowing cylinder-(E); the saidcyclone narrowing cylinder-(E) converging portion would have a greaterdiameter than the diverging portion that would enhance the air flowintensity within the said advance narrowing chamber-(F); the saidcyclone narrowing cylinder-(E) with its forward driven air stream andthe air stream would via the said advance narrowing chamber-(F); thesaid advance narrowing chamber-(F) converging portion has a greaterdiameter than the diverging portion that would enhance the air flowintensity within each one of its narrowing tube air outlets; the saidadvance narrowing chamber-(F) would contain two or a plurality of itsnarrowing tube air outlets; each one of the said advance narrowingchamber-(F) narrowing tube air outlets converging portion would have agreater diameter than the diverging portion that would to enhance thevortices intensity within the said narrowing vortex cylinder-(G); eachone of the said advance narrowing chamber-(F) narrowing tube air outletswould be connected to the said narrowing vortex cylinder-(G); each oneof the said advance narrowing chamber-(F) narrowing tube air outletscontains a vortex; the said fan chamber-(D) is connected to the saidadvance narrowing chamber-(F); the said advance narrowing chamber-(F)with its air stream would be driven by the said cyclone narrowingcylinder-(E); the said advance narrowing chamber-(F) with its air streamand the air stream would via its said narrowing tube air outlets; eachone of the said advance narrowing chamber-(F) narrowing tube air outletsis set at an angle to advance to generate and this helps to form avortex within the said narrowing vortex cylinder-(G); each one of thesaid advance narrowing chamber-(F) narrowing tube air outlets with itsair stream and the air stream would via the said narrowing vortexcylinder-(G); the said narrowing vortex cylinder-(G) would separate itscompressed air into an air-radiation heat stream and a cold stream; thesaid narrowing vortex cylinder-(G) converging portion would have agreater diameter than the diverging portion and that would enhance thevortices intensity and along with its air-radiation heat intensity ofthe vortex; the said narrowing vortex cylinder-(G) contains would avortex; the said narrowing vortex cylinder-(G) having its temperaturesand its temperatures would have a separation effect within its vortex;the said narrowing vortex cylinder-(G) with its vortex outerair-radiation heat temperature would separate from its inner cold air;the said narrowing vortex cylinder-(G) with its temperatures separationeffect would have the said vortex with an outer hot end releasing itsair-radiation heat; the said narrowing vortex cylinder-(G) with itstemperatures separation effect would have its vortex with an inner coldend releasing its cold air; the said narrowing vortex cylinder-(G) wouldhave an hot narrowing tube outlet at the outer top end of the saidnarrowing vortex cylinder-(G); the said narrowing vortex cylinder-(G)hot narrowing tube outlet converging portion would have a greaterdiameter than the diverging portion and that would enhance theair-radiation heat intensity; the said narrowing vortex cylinder-(G) hotnarrowing tube outlet would have an adjustable hot outlet valve at theouter top end of the said narrowing vortex cylinder-(G) to adjust itsair-radiation heat outward flow; the said narrowing vortex cylinder-(G)with an outer hot end releasing its air-radiation heat and theair-radiation heat would via its hot narrowing tube outlet and wouldthen via its adjustable hot outlet valve; the said narrowing vortexcylinder-(G) having its adjustable hot outlet valve with itsair-radiation heat and the air-radiation heat would via the saidradiation boiler chamber-(H); the said narrowing vortex cylinder-(G)would have an narrowing tube cold outlet near the outer top end of thesaid narrowing vortex cylinder-(G); the said narrowing vortexcylinder-(G) narrowing tube cold outlet be near the inner top end of thesaid narrowing vortex cylinder-(G); the said narrowing vortexcylinder-(G) with an inner cold end releasing its cold air and the coldair would via it's the said narrowing vortex cylinder-(G) narrowing tubecold outlet; the said narrowing vortex cylinder-(G) with its narrowingtube cold outlet and with its cold air and the cold air would via thesaid cold air cooling chamber-(J); the said air-radiation heat would belying within the said radiation boiler chamber-(H); the said radiationsteam line-(L) would be lying within the said radiation boilerchamber-(H); the said radiation steam line-(L) with its warm water andthe warm water would absorb the latent heat lying within the saidradiation boiler chamber-(H); the said warm water conversion to streamwould be lying within the said radiation steam line-(L); the saidradiation steam line-(L) would have a warm water-to-steam conversion;the said radiation boiler chamber-(H) with its air-radiation heat withinand the air-radiation heat would via its air heat outlet; the saidradiation boiler chamber-(H) with its air heat outlet with itsair-radiation heat and the now cooler air-radiation heat would exit thesaid apparatus-(A); the said cold air cooling chamber-(J) with its coldair stream and the cold air stream would absorb the latent heat from thehot water lying within the said return water line-(P); the said returnwater line-(P) would be lying within the said cold air coolingchamber-(J); the said cold air would be lying within the said cold aircooling chamber-(J); the said hot water would be lying within the saidreturn water line-(P); the said return water line-(P) would have ahot-to-warm water conversion; the said cold air cooling chamber-(J) withits cold air and the cold air would via the said flash steam cooling airchamber-(K); the said flash steam cooling air chamber-(K) with its coldair and the cold air stream would absorb the flash steam latent heatlying within the said flash steam line-chamber-(V); the said flash steamline-chamber-(V) would be lying within the said flash steam cooling airchamber-(K); the said cold air would be lying within the said flashsteam cooling air chamber-(K); said flash steam heat would be lyingwithin the said flash steam line-chamber-(V); the said flash steamline-chamber-(V) would have a steam-to-hot-warm water conversion; thesaid flash steam cooling air chamber-(K) with its cold-warm air and thecold-warm air would via its cold air outlet; the said flash steamcooling air chamber-(K) with its cold air outlet with its cold-warm airand the cold-warm air would exit the said apparatus-(A); the said warmwater pump-(R) with its warm water and then would pump the warm water tovia the said radiation steam line-(L); the said radiation steam line-(L)with its warm water-to-steam conversion and the steam would via the saidsteam turbine-(M); the said steam turbine-(M) with its steam flow wouldgenerate a rotating motion force would be forcing the said driveshaft-(N) to rotate on its horizontal-axis producing torque for the saiddrive shaft-(N) that would be joined to and would be part of the saidsteam turbine-(M); the said steam turbine-(M) would have a steam turningback to hot water conversion; the said steam turbine-(M) with its hotsteam and the hot water of the steam would via the said return waterline-(P); the hot water coming from the said steam turbine-(M) as thishot water sometimes would flash evaporation and this would also be knownas flash steam; the said return water line-(P) with its flash steam asthe flash steam would via the said flash thermostatic valve-(T) with itsdiverter valve; the said return water line-(P) with its hot water andthe hot water that did not flash evaporate to flash steam would viatoward the said warm water pump-(R); the said flash thermostaticvalve-(T) with its diverter valve and the diverter valve would divertthe flash steam to via the said flash steam line-chamber-(V); the saidflash steam that would flash evaporation is released by the said flashthermostatic valve-(T) with its diverter valve; the said flashthermostatic valve-(T) diverter valve with its flash steam and the flashsteam would via the said flash steam line-chamber-(V); the said flashsteam line-chamber-(V) with its steam-to-hot-warm water conversion andthe hot-warm water would via the said flash water pump-(W); the saidflash steam line-chamber-(V) with its steam-to-hot-warm water conversionand the hot-warm water would via the said lash water pump-(W); the saidlash water pump-(W) with its hot-warm water and the would pump thehot-warm water to via the said return water line-(P; the said flashwater pump-(W) would pump this hot-warm water to via the said returnwater line-(P toward the said warm water pump-(R); the said return waterline-(P) with its hot water and the water that did not flash to flashsteam lying within the said return water line-(P) would via toward thesaid warm water pump-(R); the said return water line-(P) with itshot-to-warm water conversion and the warm water would via the said warmwater pump-(R); the said warm water pump-(R) with its warm water andwould pump the warm water to via the said radiation steam line-(L); thepumping causes a vacuum within the said return water line-(P) anddrawing of the said water toward the said warm water pump-(R); the saidradiation steam line-(L) with its warm water-to-steam conversiontherefore commence the warm water-to-steam conversion cycle thereat. 2.An apparatus-(A) of claim 1 wherein the said apparatus-(A) would containtwo or a plurality of the narrowing spiral tube-(B) with each one withan ambient air intake and an ingrained vortex nozzle; there would be thesame amount of numbers of the said narrowing spiral tube-(B) with itsvortex nozzle as there are in numbers of the narrowing volutegenerator-(C) with its vortex nozzle; the ambient air medium being drawninto each one of the said narrowing spiral tube-(B) ambient air intakesand the air stream is being drawn in by the cyclone narrowingcylinder-(E); each one of the said narrowing spiral tube-(B) ambient airintakes is set at an angle to advance and generate and to form a vortexwithin each one of its one of the said narrowing spiral tube-(B); eachone of the said narrowing spiral tube-(B) contains a vortex; the airstream gains velocity while circumventing into the said narrowing spiraltube-(B) through its ambient air intake and is drawn circumventingthrough the said narrowing spiral tube-(B) and through its vortexnozzle; each one of the said narrowing spiral tube-(B) vortex nozzle isset at an angle to advance and generate and to form a vortex within eachone of it's one of the said narrowing volute generator-(C); each one ofthe said narrowing spiral tube-(B) converging portion has a greaterdiameter than the diverging portion to enhance the vortices intensity;each one of the said narrowing spiral tube-(B) converging portion has agreater diameter than the diverging portion to enhance the vorticesintensity within each one of it's one of the said narrowing volutegenerator-(C); the said narrowing spiral tube-(B) with its air streamand the air stream would via its said vortex nozzle; each one of thesaid narrowing spiral tube-(B) vortex nozzle with its air stream and theair stream would via it's one of the said narrowing volutegenerator-(C).
 3. An apparatus-(A) of claim 1 wherein each one of thenarrowing spiral tube-(B) vortex nozzle with its air stream the airstream would via it's one of the narrowing volute generator-(C); thesaid apparatus-(A) would contain two or a plurality of the saidnarrowing volute generator-(C) with each one with an ingrained vortexnozzle; there would be the same amount of numbers of the said narrowingvolute generator-(C) with its vortex nozzle as there are in numbers ofthe said narrowing spiral tube-(B) with its vortex nozzle; each one ofthe said narrowing volute generator-(C) converging portion has a greaterdiameter than the diverging portion to enhance its vortices intensity;each one of the said narrowing volute generator-(C) contains a vortex;the air stream is drawn circumventing into the said narrowing volutegenerator-(C) and through its vortex nozzle; the said narrowing volutegenerator-(C) air stream gains velocity while circumventing that beingdrawn through the said narrowing volute generator-(C) and through itsvortex nozzle; each one of the said narrowing volute generator-(C)vortex nozzle with its air stream and the air stream would via the fanchamber-(D).
 4. An apparatus-(A) of claim 1 wherein each one of thenarrowing volute generator-(C) vortex nozzle with its air stream and theair stream would via the fan chamber-(D); the said fan chamber-(D) isconnected to the advance narrowing chamber-(F); the cyclone narrowingcylinder-(E) joined to and would lay in-between the said fan chamber-(D)within its inner wall; the said cyclone narrowing cylinder-(E) spin onits horizontal-axis between the diameter interior side walls of the saidfan chamber-(D); the said fan chamber-(D) bottom converging portionbeing round has a greater diameter than the top portion being round thatwould enhance its air stream intensity; the said fan chamber-(D with itsair stream and the air stream would via the said cyclone narrowingcylinder-(E).
 5. An apparatus-(A) of claim 1 wherein an cyclonenarrowing cylinder-(E) converts the mechanical energy from the cylindermotor that would energize the moving air stream; the energy of the saidcylinder motor would energize the said cyclone narrowing cylinder-(E)through its rotating movement; the said cyclone narrowing cylinder-(E)air holes would energize its rotating movement with an angle to capturethe kinetic energy; the said cyclone narrowing cylinder-(E) joined toand would lay in-between the fan chamber-(D) within its inner wall; thesaid cyclone narrowing cylinder-(E) spin on its horizontal-axis betweenthe diameter interior side walls of the said fan chamber-(D); the saidcyclone narrowing cylinder-(E) would be joined to at the bottom of thesaid fan chamber-(D); the said fan chamber-(D) with its air stream andthe air stream would via the said cyclone narrowing cylinder-(E); theambient air medium being drawn into each one of the narrowing spiraltube-(B) 04 ambient air intakes and the air stream is being drawn in bythe said cyclone narrowing cylinder-(E); the air stream is then drivenby the said cyclone narrowing cylinder-(E); the said cyclone narrowingcylinder-(E) converging portion would have a greater diameter than thediverging portion to enhance the air flow intensity within the advancenarrowing chamber-(F); the said cyclone narrowing cylinder-(E) with itsforward driven air stream and the air stream would via the said advancenarrowing chamber-(F).
 6. An apparatus-(A) of claim 1 wherein an cyclonenarrowing cylinder-(E) with its forward driven air stream and the airstream would via the advance narrowing chamber-(F); the said advancenarrowing chamber-(F) converging portion has a greater diameter than thediverging portion would enhance the air flow intensity within each oneof its narrowing tube air outlets; the said advance narrowingchamber-(F) would contain two or a plurality of its narrowing tube airoutlets; each one of the said advance narrowing chamber-(F) narrowingtube air outlets converging portion would have a greater diameter thanthe diverging portion would enhance the vortices intensity within thenarrowing vortex cylinder-(G); each one of the said advance narrowingchamber-(F) narrowing tube air outlets would be connected to the saidnarrowing vortex cylinder-(G); each one of the said advance narrowingchamber-(F) narrowing tube air outlets contains a vortex; the fanchamber-(D) is connected to the said advance narrowing chamber-(F); thesaid advance narrowing chamber-(F) with its air stream would be drivenby the said cyclone narrowing cylinder-(E); the said advance narrowingchamber-(F) with its air stream and the air stream would via it's thesaid advance narrowing chamber-(F) narrowing tube air outlets; each oneof the said advance narrowing chamber-(F) narrowing tube air outlets isset at an angle to advance and generate and would help form a vortexwithin the said narrowing vortex cylinder-(G); each one of the saidadvance narrowing chamber-(F) narrowing tube air outlets with its airstream and the air stream would via the said narrowing vortexcylinder-(G).
 7. An apparatus-(A) of claim 1 wherein each one of theadvance narrowing chamber-(F) narrowing tube air outlets with its airstream and the air stream would via the narrowing vortex cylinder-(G);the said narrowing vortex cylinder-(G) would separate its compressedvortex air stream into an air-radiation heat stream and a cold stream;the said narrowing vortex cylinder-(G) converging portion would have agreater diameter than the diverging portion and would enhance thevortices intensity and along with its air-radiation heat intensity ofthe vortex; the said narrowing vortex cylinder-(G) would contains avortex; the said narrowing vortex cylinder-(G) having its temperatureswith its temperatures would have a separation effect within its vortex;the said narrowing vortex cylinder-(G) with its vortex outerair-radiation heat temperature would separate from its inner cold air;the said narrowing vortex cylinder-(G) with its temperatures separationeffect would have the said vortex with an outer hot end releasing itsair-radiation heat; the said narrowing vortex cylinder-(G) with itstemperatures separation effect and this would have its vortex with aninner cold end releasing its cold air; the said narrowing vortexcylinder-(G) would have an hot narrowing tube outlet at the outer topend of the said narrowing vortex cylinder-(G); the said narrowing vortexcylinder-(G) hot narrowing tube outlet converging portion would have agreater diameter than the diverging portion and would enhance theair-radiation heat intensity; the said narrowing vortex cylinder-(G) hotnarrowing tube outlet would have an adjustable hot outlet valve at theouter top end of the said narrowing vortex cylinder-(G) to adjust itsair-radiation heat outward flow; the said narrowing vortex cylinder-(G)with an outer hot end releasing its air-radiation heat and theair-radiation heat would via its hot narrowing tube outlet and wouldthen via its adjustable hot outlet valve; the said narrowing vortexcylinder-(G) having its adjustable hot outlet valve with itsair-radiation heat and the air-radiation heat would via the radiationboiler chamber-(H); the said narrowing vortex cylinder-(G) would have annarrowing tube cold outlet near the outer top end of the said narrowingvortex cylinder-(G); the said narrowing vortex cylinder-(G) would havenarrowing tube cold outlet with its adjustable hot outlet valve; thesaid narrowing vortex cylinder-(G) with an inner cold end releasing itscold air and the cold air would via it's the said narrowing vortexcylinder-(G) narrowing tube cold outlet; the said narrowing vortexcylinder-(G) with its narrowing tube cold outlet with its cold air andthe cold air would via the cold air cooling chamber-(J).
 8. Anapparatus-(A) of claim 1 wherein an narrowing vortex cylinder-(G) havingits adjustable hot outlet valve with its air-radiation heat and theair-radiation heat would via the radiation boiler chamber-(H); theradiation steam line-(L) would be lying within the said radiation boilerchamber-(H); the said radiation steam line-(L) with its warm water andthe warm water would absorb the latent heat lying within the saidradiation boiler chamber-(H); the said air-radiation heat would be lyingwithin the said radiation boiler chamber-(H); the said warm waterconversion to stream would be lying within the said radiation steamline-(L); the said radiation steam line-(L) would have a warmwater-to-steam conversion; the said radiation boiler chamber-(H) withits air-radiation heat within and the air-radiation heat would via itsair heat outlet; the said radiation boiler chamber-(H) with its air heatoutlet with its air-radiation heat and the now cooler air-radiation heatwould exit the said apparatus-(A).
 9. An apparatus-(A) of claim 1wherein an the narrowing vortex cylinder-(G) with its narrowing tubecold outlet with its cold air and the cold air would via the cold aircooling chamber-(J); the return water line-(P) would be lying within thesaid cold air cooling chamber-(J); the said cold air cooling chamber-(J)with its cold air stream and the cold air stream would absorb the latentheat from the hot water lying within the said return water line-(P); thesaid cold air would be lying within the said cold air coolingchamber-(J); the said hot water would be lying within the said returnwater line-(P); the said return water line-(P) would have a hot-to-warmwater conversion; the said cold air cooling chamber-(J) with its coldair and the cold air would via the flash steam cooling air chamber-(K).10. An apparatus-(A) of claim 1 wherein the cold air cooling chamber-(J)with its cold air and the cold air would via the flash steam cooling airchamber-(K); the flash steam line-chamber-(V) would be lying within thesaid flash steam cooling air chamber-(K); the said flash steam coolingair chamber-(K) with its cold air and the cold air stream would absorbthe flash steam latent heat lying within the said flash steamline-chamber-(V); the said cold air would be lying within the said flashsteam cooling air chamber-(K); the said flash steam heat would be lyingwithin the said flash steam line-chamber-(V); the said flash steamline-chamber-(V) would have a steam-to-hot-warm water conversion; thesaid flash steam cooling air chamber-(K) with its cold-warm air and thecold-warm air would via its cold air outlet; the said flash steamcooling air chamber-(K) with its cold air outlet with its cold-warm airand the cold-warm air would exit the said apparatus-(A).
 11. Anapparatus-(A) of claim 1 wherein the warm water pump-(R) with its warmwater and pumps the warm water to via the radiation steam line-(L); thesaid radiation steam line-(L) would be lying within the radiation boilerchamber-(H); the said radiation steam line-(L) with its warm water andthe warm water would absorb the latent heat lying within the saidradiation boiler chamber-(H); the said air-radiation heat would be lyingwithin the said radiation boiler chamber-(H); the said warm waterconversion to stream would be lying within the said radiation steamline-(L); the said radiation steam line-(L) would have a warmwater-to-steam conversion; the said radiation steam line-(L) with itswarm water-to-steam conversion and the steam would via the steamturbine-(M).
 12. An apparatus-(A) of claim 1 wherein the radiation steamline-(L) with its warm water-to-steam conversion and the steam would viathe steam turbine-(M); the said steam turbine-(M) with its steam flowwould generate a rotating motion force and forcing the drive shaft-(N)to rotate on its horizontal-axis producing torque; the said driveshaft-(N) would be joined to and that being part of the said steamturbine-(M); the said steam turbine-(M) would have a steam turning backto hot water conversion; the said steam turbine-(M) with its hot steamand the hot water of the steam would via the return water line-(P). 13.An apparatus-(A) of claim 1 wherein the steam turbine-(M) with its steamflow would generate a rotating motion force and forcing the driveshaft-(N) to rotate on its horizontal-axis producing torque; the saiddrive shaft-(N) would be joined to and being part of the said steamturbine-(M).
 14. An apparatus-(A) of claim 1 wherein the steamturbine-(M) with its hot steam and the hot water of the steam would viathe return water line-(P); the hot water coming from the said steamturbine-(M) and this hot water sometimes would flash evaporation andwould be also known as flash steam; the said return water line-(P) withits flash steam and the flash steam would via the flash thermostaticvalve-(T) with its diverter valve; the said return water line-(P) withits hot water and the hot water that did not flash evaporate to flashsteam would via toward the warm water pump-(R).
 15. An apparatus-(A) ofclaim 1 wherein an the return water line-(P) with its flash steam andthe flash steam would via the flash thermostatic valve-(T) with itsdiverter valve; the said flash thermostatic valve-(T) with its divertervalve and the diverter valve would divert the flash steam to via theflash steam line-chamber-(V); the flash steam that would flashevaporation is released by the said flash thermostatic valve-(T) withits diverter valve; the said flash thermostatic valve-(T) diverter valvewith its flash steam and the flash steam would via the said flash steamline-chamber-(V).
 16. An apparatus-(A) of claim 1 wherein the flashthermostatic valve-(T) diverter valve with its flash steam and the flashsteam would via the flash steam line-chamber-(V); the flash steamcooling air chamber-(K) would be lying within the said flash steamline-chamber-(V); the said flash steam cooling air chamber-(K) with itscold air and the cold air stream would absorb the flash steam latentheat lying within the said flash steam line-chamber-(V); the said coldair would be lying within the said flash steam cooling air chamber-(K);the said flash steam heat would be lying within the said flash steamline-chamber-(V); the said flash steam line-chamber-(V) would have asteam-to-hot-warm water conversion; the said flash steamline-chamber-(V) with its steam-to-hot-warm water conversion and thehot-warm water would via the flash water pump-(W).
 17. An apparatus-(A)of claim 1 wherein the flash steam line-chamber-(V) with itssteam-to-hot-warm water conversion and the hot-warm water would via theflash water pump-(W); the said flash water pump-(W) with its hot-warmwater and pumps the hot-warm water to via the return water line-(P); thesaid flash water pump-(W) would pump this hot-warm water to via the saidreturn water line-(P) toward the warm water pump-(R).
 18. Anapparatus-(A) of claim 1 wherein an flash water pump-(W) with itshot-warm water and pumps the hot-warm water to via the return waterline-(P); the said return water line-(P) with its hot water and thewater that did not flash to flash steam lying within the said returnwater line-(P) would via toward the warm water pump-(R); the said returnwater line-(P) would be lying within the cold air cooling chamber-(J);the said cold air cooling chamber-(J) with its cold air stream and thecold air stream would absorb the latent heat from the hot water lyingwithin the said return water line-(P); the said cold air would be lyingwithin the said cold air cooling chamber-(J); the said hot water wouldbe lying within the said return water line-(P); the said return waterline-(P) would have a hot-to-warm water conversion; the said returnwater line-(P) with its hot-to-warm water conversion and the warm waterwould via the said warm water pump-(R).
 19. An apparatus-(A) of claim 1wherein the return water line-(P) with its hot water-to-warm water andthe warm water would via toward the warm water pump-(R); the said warmwater pump-(R) with its warm water and pumps the warm water to via theradiation steam line-(L); the pumping causes a vacuum within the saidreturn water line-(P) and would draw the said water toward the said warmwater pump-(R); the said radiation steam line-(L) with its warmwater-to-steam conversion therefore commence the warm water-to-steamconversion cycle thereat.
 20. An apparatus-NVCHACR-(NV) accelerate airstream to form and producing an fast moving vortex air producing to havean temperatures separation effect having its air-radiation heat separatefrom its air stream producing the separated high temperatures and coldtemperatures; the said apparatus-NVCHACR-(NV) is a closed area with anopening at each one of the narrowing spiral tube-(B) at its ambient airintakes and the narrowing vortex cylinder-(G) at its narrowing tube coldoutlet and the said narrowing vortex cylinder-(G) at its adjustable hotoutlet valve; the said apparatus-NVCHACR-(NV) would contain two or aplurality of the said narrowing spiral tube-(B) with each one with anambient air intake and an ingrained vortex nozzle; the ambient airmedium being drawn into each one of the said narrowing spiral tube-(B)ambient air intakes and the air stream is being drawn in by the cyclonenarrowing cylinder-(E); each one of the said narrowing spiral tube-(B)ambient air intakes is set at an angle to advance and generate and toform a vortex within each one of its one of the said narrowing spiraltube-(B); each one of the said narrowing spiral tube-(B) contains avortex; the air stream gains velocity while circumventing into the saidnarrowing spiral tube-(B) through its ambient air intake and is drawncircumventing through the said narrowing spiral tube-(B) and through itsvortex nozzle; each one of the said narrowing spiral tube-(B) vortexnozzle is set at an angle to advance and generate and would form avortex within each one of it's one of the narrowing volutegenerator-(C); each one of the said narrowing spiral tube-(B) convergingportion has a greater diameter than the diverging portion and to enhancethe vortices intensity; each one of the said narrowing spiral tube-(B)converging portion has a greater diameter than the diverging portion andto enhance the vortices intensity within each one of it's one of thesaid narrowing volute generator-(C); the said narrowing spiral tube-(B)with its air stream and the air stream would via its said vortex nozzle;each one of the said narrowing spiral tube-(B) vortex nozzle with itsair stream and the air stream would via within each of its own one ofthe said narrowing volute generator-(C); there would be the same amountof numbers of the said narrowing spiral tube-(B) with its vortex nozzleas there are in numbers of the said narrowing volute generator-(C) withits vortex nozzle; each one of the said narrowing spiral tube-(B) vortexnozzle with its air stream and the air stream would via it's one of thesaid narrowing volute generator-(C); the said apparatus-NVCHACR-(NV)would contain two or a plurality of the said narrowing volutegenerator-(C) with each one with an ingrained vortex nozzle; there wouldbe the same amount of numbers of the said narrowing volute generator-(C)with its vortex nozzle as there are in numbers of the said narrowingspiral tube-(B) with its vortex nozzle; each one of the said narrowingvolute generator-(C) converging portion has a greater diameter than thediverging portion to enhance its vortices intensity; each one of thesaid narrowing volute generator-(C) contains a vortex; the air stream isdrawn circumventing into the said narrowing volute generator-(C) andthrough its vortex nozzle; the said narrowing volute generator-(C) airstream gains velocity while circumventing and being drawn through thesaid narrowing volute generator-(C) and through its vortex nozzle; eachone of the said narrowing volute generator-(C) vortex nozzle with itsair stream and the air stream would via the fan chamber-(D); each one ofthe said narrowing volute generator-(C) vortex nozzle with its airstream and the air stream would via the said fan chamber-(D); the saidfan chamber-(D) is connected to the advance narrowing chamber-(F); thesaid cyclone narrowing cylinder-(E) joined to and would lay in-betweenthe said fan chamber-(D) within its inner wall; the said cyclonenarrowing cylinder-(E) spin on its horizontal-axis between the diameterinterior side walls of the said fan chamber-(D); the said fanchamber-(D) bottom converging portion being round has a greater diameterthan the top portion being round to enhance its air stream intensity;the said cyclone narrowing cylinder-(E) converts the mechanical energyfrom the cylinder motor and to energize the moving air stream; theenergy of the said cylinder motor would energize the said cyclonenarrowing cylinder-(E) through its rotating movement; the said cyclonenarrowing cylinder-(E) air holes would energize its rotating movementwith an angle to capture the kinetic energy; the said cyclone narrowingcylinder-(E) joined to and would lay in-between the said fan chamber-(D)within its inner wall; the said cyclone narrowing cylinder-(E) spin onits horizontal-axis between the diameter interior side walls of the saidfan chamber-(D); the said cyclone narrowing cylinder-(E) would be joinedto at the bottom of the said fan chamber-(D); the said fan chamber-(D)with its air stream and the air stream would via the said cyclonenarrowing cylinder-(E); the ambient air medium being drawn into each oneof the said narrowing spiral tube-(B) ambient air intakes and the airstream is being drawn in by the said cyclone narrowing cylinder-(E); theair stream is then driven by the said cyclone narrowing cylinder-(E);the said cyclone narrowing cylinder-(E) converging portion would have agreater diameter than the diverging portion and to enhance the air flowintensity within the said advance narrowing chamber-(F); the saidcyclone narrowing cylinder-(E) with its forward driven air stream andthe air stream would via the said advance narrowing chamber-(F); thesaid cyclone narrowing cylinder-(E) with its forward driven air streamand the air stream would via the said advance narrowing chamber-(F); thesaid advance narrowing chamber-(F) converging portion has a greaterdiameter than the diverging portion and to enhance the air flowintensity within each one of its narrowing tube air outlets; the saidadvance narrowing chamber-(F) would contain two or a plurality of itsnarrowing tube air outlets; each one of the said advance narrowingchamber-(F) narrowing tube air outlets converging portion would have agreater diameter than the diverging portion and to enhance the vorticesintensity within the narrowing vortex cylinder-(G); each one of the saidadvance narrowing chamber-(F) narrowing tube air outlets would beconnected to the said narrowing vortex cylinder-(G); each one of thesaid advance narrowing chamber-(F) narrowing tube air outlets contains avortex; the said fan chamber-(D) is connected to the said advancenarrowing chamber-(F); the said advance narrowing chamber-(F) with itsair stream would be driven by the said cyclone narrowing cylinder-(E);the said advance narrowing chamber-(F) with its air stream and the airstream would via it's the said advance narrowing chamber-(F) narrowingtube air outlets; each one of the said advance narrowing chamber-(F)narrowing tube air outlets is set at an angle to advance and generateand would help to form a vortex within the said narrowing vortexcylinder-(G); each one of the said advance narrowing chamber-(F)narrowing tube air outlets with its air stream and the air stream wouldvia the said narrowing vortex cylinder-(G); each one of the said advancenarrowing chamber-(F) narrowing tube air outlets with its air stream andthe air stream would via the said narrowing vortex cylinder-(G); thesaid narrowing vortex cylinder-(G) would separate its compressed vortexair stream into an air-radiation heat stream and a cold stream; the saidnarrowing vortex cylinder-(G) converging portion would have a greaterdiameter than the diverging portion and to enhance the vorticesintensity and along with its air-radiation heat intensity of the vortex;the said narrowing vortex cylinder-(G) contains a vortex; the saidnarrowing vortex cylinder-(G) having its temperatures and itstemperatures would have a separation effect within its vortex; the saidnarrowing vortex cylinder-(G) with its vortex outer air-radiation heattemperature would separate from its inner cold air; the said narrowingvortex cylinder-(G) with its temperatures separation effect would havethe said vortex with an outer hot end releasing its air-radiation heat;the said narrowing vortex cylinder-(G) with its temperatures separationeffect and this would have its vortex with an inner cold end releasingits cold air; the said narrowing vortex cylinder-(G) would have an hotnarrowing tube outlet at the outer top end of the said narrowing vortexcylinder-(G); the said narrowing vortex cylinder-(G) hot narrowing tubeoutlet converging portion would have a greater diameter than thediverging portion would enhance the air-radiation heat intensity; thesaid narrowing vortex cylinder-(G) hot narrowing tube outlet would havean adjustable hot outlet valve at the outer top end of the saidnarrowing vortex cylinder-(G) to adjust its air-radiation heat outwardflow; the said narrowing vortex cylinder-(G) with an outer hot endreleasing its air-radiation heat and the air-radiation heat would viaits hot narrowing tube outlet and would then via its adjustable hotoutlet valve; the said narrowing vortex cylinder-(G) having itsadjustable hot outlet valve with its air-radiation heat and theair-radiation heat would exit the said apparatus-NVCHACR-(NV); the saidnarrowing vortex cylinder-(G) would have an narrowing tube cold outletnear the outer top end of the said narrowing vortex cylinder-(G); thesaid narrowing vortex cylinder-(G) with an inner cold end releasing itscold air and the cold air would via it's the said narrowing vortexcylinder-(G) narrowing tube cold outlet; the said narrowing vortexcylinder-(G) with its narrowing tube cold outlet with its cold air andthe cold air would exit the said apparatus-NVCHACR-(NV).